Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restrictive measures against Iran and repealing Regulation (EU) No 961/2010

Council Regulation (EU) No 267/2012of 23 March 2012concerning restrictive measures against Iran and repealing Regulation (EU) No 961/2010 CHAPTER IDEFINITIONS

Article 1For the purposes of this Regulation the following definitions shall apply:(a)'branch' of a financial or credit institution means a place of business which forms a legally dependent part of a financial or credit institution and which carries out directly all or some of the transactions inherent in the business of financial or credit institutions;(b)'brokering services' means:(i)the negotiation or arrangement of transactions for the purchase, sale or supply of goods and technology or of financial and technical services, including from a third country to any other third country, or(ii)the selling or buying of goods and technology or of financial and technical services, including where they are located in third countries for their transfer to another third country;(c)'claim' means any claim, whether asserted by legal proceedings or not, made before or after the date of entry into force of this Regulation, under or in connection with a contract or transaction, and includes in particular:(i)a claim for performance of any obligation arising under or in connection with a contract or transaction;(ii)a claim for extension or payment of a bond, financial guarantee or indemnity of whatever form;(iii)a claim for compensation in respect of a contract or transaction;(iv)a counterclaim;(v)a claim for the recognition or enforcement, including by the procedure of exequatur, of a judgment, an arbitration award or an equivalent decision, wherever made or given;(d)'contract or transaction' means any transaction of whatever form and whatever the applicable law, whether comprising one or more contracts or similar obligations made between the same or different parties; for this purpose 'contract' includes a bond, guarantee or indemnity, particularly a financial guarantee or financial indemnity, and credit, whether legally independent or not, as well as any related provision arising under, or in connection with, the transaction;(e)'competent authorities' refers to the competent authorities of the Member States as identified on the websites listed in Annex X;(f)'credit institution' means a credit institution as defined in Article 4(1) of Directive 2006/48/EC of the European Parliament and of the Council of 14 June 2006 relating to the taking up and pursuit of the business of credit institutionsOJ L 177, 30.6.2006, p. 1., including its branches inside or outside the Union;(g)'customs territory of the Union' means the territory as defined in Article 3 of Council Regulation (EEC) No 2913/92 of 12 October 1992 establishing the Community Customs CodeOJ L 302, 19.10.1992, p. 1. and in Commission Regulation (EEC) No 2454/93 of 2 July 1993 laying down provisions for the implementation of Regulation (EEC) No 2913/92OJ L 253, 11.10.1993, p. 1.;(h)'economic resources' means assets of every kind, whether tangible or intangible, movable or immovable, which are not funds, but which may be used to obtain funds, goods or services;(i)'financial institution' means(i)an undertaking, other than a credit institution, which carries out one or more of the operations included in points 2 to 12 and points 14 and 15 of Annex I to Directive 2006/48/EC, including the activities of currency exchange offices (bureaux de change);(ii)an insurance company duly authorised in accordance with Directive 2009/138/EC of the European Parliament and of the Council of 25 November 2009 on the taking-up and pursuit of the business of Insurance and Reinsurance (Solvency II)OJ L 335, 17.12.2009, p. 1., in so far as it carries out activities covered by that Directive;(iii)an investment firm as defined in point 1 of Article 4(1) of Directive 2004/39/EC of the European Parliament and of the Council of 21 April 2004 on markets in financial instrumentsOJ L 145, 30.4.2004, p. 1.;(iv)a collective investment undertaking marketing its units or shares; or(v)an insurance intermediary as defined in Article 2(5) of Directive 2002/92/EC of the European Parliament and of the Council of 9 December 2002 on insurance mediationOJ L 9, 15.1.2003, p. 3., with the exception of intermediaries referred to in Article 2(7) of that Directive, when they act in respect of life insurance and other investment related services;including its branches inside or outside the Union;(j)'freezing of economic resources' means preventing the use of economic resources to obtain funds, goods or services in any way, including, but not limited to, by selling, hiring or mortgaging them;(k)'freezing of funds' means preventing any move, transfer, alteration, use of, access to, or dealing with funds in any way that would result in any change in their volume, amount, location, ownership, possession, character, destination or other change that would enable the funds to be used, including portfolio management;(l)'funds' means financial assets and benefits of every kind, including, but not limited to:(i)cash, cheques, claims on money, drafts, money orders and other payment instruments;(ii)deposits with financial institutions or other entities, balances on accounts, debts and debt obligations;(iii)publicly-and privately-traded securities and debt instruments, including stocks and shares, certificates representing securities, bonds, notes, warrants, debentures and derivatives contracts;(iv)interest, dividends or other income on or value accruing from or generated by assets;(v)credit, right of set-off, guarantees, performance bonds or other financial commitments;(vi)letters of credit, bills of lading, bills of sale; and(vii)documents showing evidence of an interest in funds or financial resources;(m)'goods' includes items, materials and equipment;(n)'insurance' means an undertaking or commitment whereby one or more natural or legal persons is or are obliged, in return for a payment, to provide one or more other persons, in the event of materialisation of a risk, with an indemnity or a benefit as determined by the undertaking or commitment;(o)'Iranian person, entity or body' means:(i)the State of Iran or any public authority thereof;(ii)any natural person in, or resident in, Iran;(iii)any legal person, entity or body having its registered office in Iran;(iv)any legal person, entity or body, inside or outside Iran, owned or controlled directly or indirectly by one or more of the above mentioned persons or bodies;(p)'reinsurance' means the activity consisting in accepting risks ceded by an insurance undertaking or by another reinsurance undertaking or, in the case of the association of underwriters known as Lloyd's, the activity consisting in accepting risks, ceded by any member of Lloyd's, by an insurance or reinsurance undertaking other than the association of underwriters known as Lloyd's;(q)'Sanctions Committee' means the Committee of the United Nations Security Council which was established pursuant to paragraph 18 of United Nations Security Council Resolution ("UNSCR") 1737 (2006);(r)'technical assistance' means any technical support related to repairs, development, manufacture, assembly, testing, maintenance, or any other technical service, and may take forms such as instruction, advice, training, transmission of working knowledge or skills or consulting services; including verbal forms of assistance;(s)'territory of the Union' means the territories of the Member States to which the Treaty is applicable, under the conditions laid down in the Treaty, including their airspace;(t)'transfer of funds' means:(i)any transaction carried out on behalf of a payer through a payment service provider by electronic means, with a view to making funds available to a payee at a payment service provider, irrespective of whether the payer and the payee are the same person. The terms payer, payee and payment service provider have the same meaning as in Directive 2007/64/EC of the European Parliament and of the Council of 13 November 2007 on payment services in the internal marketOJ L 319, 5.12.2007, p. 1.;(ii)any transaction by non-electronic means such as in cash, cheques or accountancy orders, with a view to making funds available to a payee irrespective of whether the payer and the payee are the same person.(u)'Joint Commission' means a joint commission consisting of representatives of Iran and of China, France, Germany, the Russian Federation, the United Kingdom and the United States with the High Representative of the Union for Foreign Affairs and Security Policy ("High Representative"), that will be established to monitor the implementation of the Joint Comprehensive Plan of Action of 14 July 2015 ("JCPOA") and will carry out the functions provided for in the JCPOA, in accordance with point ix of the JCPOA's "Preamble and General Provisions" and Annex IV to the JCPOA.

CHAPTER IIEXPORT AND IMPORT RESTRICTIONS

Article 21.It shall be prohibited to sell, supply, transfer or export, directly or indirectly, the goods and technology listed in Annex I or II, whether or not originating in the Union, to any Iranian person, entity or body or for use in Iran.2.Annex I shall include goods and technology, including software, which are dual-use items or technology as defined in Regulation (EC) No 428/2009, except for certain goods and technology as specified in part A of Annex I to this Regulation.2a.The Member State concerned shall inform the other Member States and the Commission, within four weeks, of authorisations granted in accordance with Regulation (EC) No 428/2009, in respect of the goods and technology as specified in part A of Annex I to this Regulation.3.Annex II shall include other goods and technology which could contribute to Iran's enrichment-related, reprocessing or heavy-water-related activities, to the development of nuclear weapon delivery systems, or to the pursuit of activities related to other topics about which the International Atomic Energy Agency (IAEA) has expressed concerns or has identified as outstanding, including those determined by the UN Security Council or by the Sanctions Committee.4.Annexes I and II shall not include goods and technology included in the Common Military List of the European UnionOJ C 69, 18.3.2010, p. 19. ('Common Military List').

Article 31.A prior authorisation shall be required for the sale, supply, transfer or export, directly or indirectly, of the goods and technology listed in Annex III, whether or not originating in the Union, to any Iranian person, entity or body or for use in Iran.2.For all exports for which an authorisation is required under this Article, such authorisation shall be granted by the competent authorities of the Member State where the exporter is established and shall be in accordance with the detailed rules laid down in Article 11 of Regulation (EC) No 428/2009. The authorisation shall be valid throughout the Union.3.Annex III shall include any goods and technology, other than those included in Annexes I and II, which could contribute to enrichment-related, reprocessing or heavy water-related activities, to the development of nuclear weapon delivery systems, or to the pursuit of activities related to other topics about which the IAEA has expressed concerns or has identified as outstanding.4.Exporters shall supply the competent authorities with all relevant information required for their application for an export authorisation.5.The competent authorities shall not grant any authorisation for any sale, supply, transfer or export of the goods or technology included in Annex III, if they have reasonable grounds to determine that the sale, supply, transfer or export of the goods and technology is or may be intended for use in connection with one of the following activities:(a)Iran's enrichment-related, reprocessing or heavy water-related activities;(b)the development of nuclear weapon delivery systems by Iran; or(c)the pursuit by Iran of activities related to other topics about which the IAEA has expressed concerns or has identified as outstanding.6.Under the conditions set out in paragraph 5, the competent authorities may annul, suspend, modify or revoke an export authorisation which they have granted.7.Where a competent authority refuses to grant an authorisation, or annuls, suspends, substantially limits or revokes an authorisation in accordance with paragraphs 5 or 6, the Member State concerned shall notify the other Member States and the Commission thereof and share the relevant information with them, while complying with the provisions concerning the confidentiality of such information of Council Regulation (EC) No 515/97 of 13 March 1997 on mutual assistance between the administrative authorities of the Member States and cooperation between the latter and the Commission to ensure the correct application of the law on customs and agricultural mattersOJ L 82, 22.3.1997, p. 1..8.Before a Member State grants an authorisation in accordance with paragraph 5 for a transaction which is essentially identical to a transaction which is the subject of a still valid denial issued by another Member State or by other Member States under paragraphs 6 and 7, it shall first consult the Member State or States which issued the denial. If, following such consultations, the Member State concerned decides to grant an authorisation, it shall inform the other Member States and the Commission thereof, providing all relevant information to explain the decision.

Article 4It shall be prohibited to purchase, import or transport from Iran, directly or indirectly, the goods and technology listed in Annex I or II whether the item concerned originates in Iran or not.

Article 2a1.A prior authorisation shall be required:(a)for the sale, supply, transfer or export, directly or indirectly, of the goods and technology listed in Annex I, whether or not originating in the Union, to any Iranian person, entity or body or for use in Iran;(b)for the provision of technical assistance or brokering services related to goods and technology listed in Annex I or related to the provision, manufacture, maintenance and use of goods and technology included in Annex I, directly or indirectly, to any Iranian person, entity or body, or for use in Iran;(c)for the provision of financing or financial assistance related to goods and technology listed Annex I, including in particular grants, loans and export credit insurance for any sale, supply, transfer or export of such items, or for any provision of related technical assistance or brokering services, directly or indirectly, to any Iranian person, entity or body, or for use in Iran;(d)before entering into any arrangement with an Iranian person, entity or body, or any person or entity acting on their behalf or at their direction, including the acceptance of loans or credit made by such person, entity or body, that would enable such person, entity or body to participate in or increase its participation, be that independently or as part of a joint venture or other partnership, in commercial activities involving the following:(i)uranium mining,(ii)production or use of nuclear materials as listed in Part 1 of the Nuclear Suppliers Group list.This shall include the making of loans or credit to such a person, entity or body;(e)for the purchase, import or transport from Iran of goods and technology listed in Annex I, whether or not originating in Iran.2.Annex I shall list the items, including goods, technology and software, contained in the Nuclear Suppliers Group list.3.The Member State concerned shall submit the proposed authorisation under points (a) to (d) of paragraph 1 to the UN Security Council for approval on a case-by-case basis and shall not grant the authorisation until that approval has been received.4.The Member State concerned shall also submit the proposed authorisations of activities referred to in points (a) to (d) of paragraph 1 to the UN Security Council for approval on a case-by-case basis if the activities are related to any further goods and technology that, based on the determination by that Member State, could contribute to reprocessing- or enrichment-related or heavy water-related activities inconsistent with the JCPOA. The Member State shall not grant the authorisation until that approval has been received.5.The Member State concerned shall notify the Joint Commission of authorisations granted under point (e) of paragraph 1 and authorisations concerning the purchase, import or transport from Iran of the further goods and technology referred to in paragraph 4, whether or not originating in Iran.6.The Member State concerned shall notify the other Member States, the Commission and the High Representative of authorisations granted under paragraphs (1) and (5), or any refusal by the UN Security Council to approve an authorisation in accordance with paragraphs (3) or (4).

Article 2b1.Article 2a(3) and (4) do not apply in relation to proposed authorisations for the supply, sale or transfer to Iran of equipment referred to in paragraph 2(c), subparagraph 1 of Annex B to UNSCR 2231 (2015) for light water reactors.2.The Member State concerned shall inform the other Member States, the Commission and the High Representative, within four weeks, of authorisations granted under this Article.

Article 2c1.The competent authorities granting an authorisation in accordance with Article 2a(1)(a) and Article 2b shall ensure the following:(a)the requirements, as appropriate, of the Guidelines as set out in the Nuclear Suppliers Group list have been met;(b)the rights to verify the end-use and end-use location of any supplied item have been obtained from Iran and can be exercised effectively;(c)the notification of the UN Security Council within ten days of the supply, sale or transfer; and(d)in the case of supplied goods and technology referred to in Annex I, the notification of the IAEA within ten days of the supply, sale or transfer.2.For all exports for which an authorisation is required under Article 2a(1)(a), such authorisation shall be granted by the competent authorities of the Member State where the exporter is established. The authorisation shall be valid throughout the Union.3.Exporters shall supply the competent authorities with all relevant information, as set out in Article 14(1) of Regulation (EC) No 428/2009 and as specified by each competent authority, required for their application for an export authorisation.

Article 2d1.Article 2a(3) and (4) do not apply in relation to proposed authorisations for the supply, sale, or transfer of items, materials, equipment, goods and technology, and the provision of any related technical assistance, training, financial assistance, investment, brokering or other services where the competent authorities consider them to be directly related to the following:(a)the necessary modification of two cascades at the Fordow facility for stable isotope production;(b)the export of Iran's enriched uranium in excess of 300 kilograms in return for natural uranium; or(c)the modernisation of the Arak reactor based on the agreed conceptual design and, subsequently, on the agreed final design of such reactor.2.The competent authority granting an authorisation in accordance with paragraph 1 shall ensure the following:(a)all activities are undertaken strictly in accordance with the JCPOA;(b)the requirements, as appropriate, of the Guidelines as set out in the Nuclear Suppliers Group list have been met;(c)rights to verify the end-use and end-use location of any supplied item have been obtained from Iran and can be exercised effectively.3.The Member State concerned shall notify:(a)the UN Security Council and the Joint Commission ten days in advance of such activities;(b)the IAEA within ten days of the supply, sale or transfer, in case of supplied items, materials, equipment, goods and technology included in the Nuclear Suppliers Group list.4.The Member State concerned shall inform the other Member States, the Commission and the High Representative, within four weeks, of authorisations granted under this Article.

Article 3a1.A prior authorisation shall be required, on a case-by-case basis:(a)for the sale, supply, transfer or export, directly or indirectly, of the goods and technology listed in Annex II, whether or not originating in the Union, to any Iranian person, entity or body or for use in Iran;(b)for the provision of technical assistance or brokering services related to goods and technology listed in Annex II or related to the provision, manufacture, maintenance and use of goods included in Annex II, directly or indirectly, to any Iranian person, entity or body, or for use in Iran;(c)for the provision of financing or financial assistance related to goods and technology listed Annex II, including in particular grants, loans and export credit insurance for any sale, supply, transfer or export of such items, or for any provision of related technical assistance or brokering services, directly or indirectly, to any Iranian person, entity or body, or for use in Iran;(d)before entering into any arrangement with an Iranian person, entity or body, or any person or entity acting on their behalf or at their direction, including the acceptance of loans or credit made by such person, entity or body, that would enable such person, entity or body to participate in or increase its participation, be that independently or as part of a joint venture or other partnership, in commercial activities involving technologies listed in Annex II.;(e)for the purchase, import or transport from Iran of goods and technology listed in Annex II, whether or not originating in Iran.2.Annex II shall list the goods and technology, other than those included in Annexes I and III, that could contribute to reprocessing- or enrichment-related or heavy water-related or other activities inconsistent with the JCPOA.3.Exporters shall supply the competent authorities with all relevant information required for their application for an authorisation.4.The competent authorities shall not grant any authorisation for the transactions referred to in paragraph 1(a) to (e), if they have reasonable grounds to determine that the actions concerned would contribute to reprocessing- or enrichment-related, heavy water-related or other nuclear related activities inconsistent with the JCPOA.5.The competent authorities shall exchange information on requests for authorisation received under this Article. The system referred to in Article 19(4) of Regulation (EC) No 428/2009 shall be used for this purpose.6.The competent authority granting an authorisation in accordance with paragraph 1(a) shall ensure that, except for temporary exports, the applicant has submitted the end-use statement set out in Annex IIa or an end-use statement in an equivalent document containing information on the end-use and, as a basic principle, end-use location of any supplied item.6a.If the competent authority decides to grant an authorisation in accordance with paragraph 1(a) in the absence of information on the end-use location, it may request the applicant to supply such information at a later stage. The applicant shall provide the information within a reasonable period of time.7.The Member State concerned shall notify the other Member States, the Commission and the High Representative of its intention to grant an authorisation under this Article at least ten days prior to the authorisation.

Article 3b1.For all exports for which an authorisation is required under Article 3a, such authorisation shall be granted by the competent authorities of the Member State where the exporter is established and shall be in accordance with the detailed rules laid down in Article 11 of Regulation (EC) No 428/2009. The authorisation shall be valid throughout the Union.2.Under the conditions set out in Article 3a(4) and (5), the competent authorities may annul, suspend, modify or revoke an export authorisation which they have granted.3.Where a competent authority refuses to grant an authorisation, or annuls, suspends, substantively modifies or revokes an authorisation in accordance with Article 3a(4), the Member State concerned shall notify the other Member States, the Commission and the High Representative thereof and share the relevant information with them, while complying with the provisions concerning the confidentiality of such information of Council Regulation (EC) No 515/97Council Regulation (EC) No 515/97 of 13 March 1997 on mutual assistance between the administrative authorities of the Member States and cooperation between the latter and the Commission to ensure the correct application of the law on customs and agricultural matters (OJ L 82, 22.3.1997, p. 1)..4.Before a competent authority of a Member State grants an authorisation in accordance with Article 3a for a transaction which is essentially identical to a transaction which is the subject of a still valid denial issued by another Member State or by other Member States under Article 3a(4), it shall first consult the Member State or Member States which issued the denial. If, following such consultations, the Member State concerned decides to grant an authorisation, it shall inform the other Member States, the Commission and the High Representative thereof, providing all relevant information to explain the decision.

Article 3c1.Article 3a does not apply in relation to proposed authorisations for the supply, sale or transfer to Iran of goods and technology listed in Annex II for light water reactors.2.The competent authority granting an authorisation in accordance with paragraph 1 shall ensure that, except for temporary exports, the applicant has submitted the end-use statement set out in Annex IIa or an end-use statement in an equivalent document containing information on the end-use and, as a basic principle, end-use location of any supplied item.2a.If the competent authority decides to grant an authorisation in accordance with paragraph 1(a) in the absence of information on the end-use location, it may request the applicant to supply such information at a later stage. The applicant shall provide the information within a reasonable period of time.3.The Member State concerned shall inform the other Member States, the Commission and the High Representative, within four weeks, of authorisations granted under this Article.

Article 3d1.Article 3a does not apply in relation to proposed authorisations for the supply, sale, or transfer of items, materials, equipment, goods and technology, and the provision of any related technical assistance, training, financial assistance, investment, brokering or other services where the competent authorities consider them to be directly related to the following:(a)the necessary modification of two cascades at the Fordow facility for stable isotope production;(b)the export of Iran's enriched uranium in excess of 300 kilograms in return for natural uranium; or(c)the modernisation of the Arak reactor based on the agreed conceptual design and, subsequently, on the agreed final design of such reactor.2.The competent authority granting an authorisation in accordance with paragraph 1 shall ensure that:(a)all activities are undertaken strictly in accordance with the JCPOA; and(b)except for temporary exports, the applicant has submitted the end-use statement set out in Annex IIa or an end-use statement in an equivalent document containing information on the end-use and, as a basic principle, end-use location of any supplied item.2a.If the competent authority decides to grant an authorisation in accordance with paragraph 1(a) in the absence of information on the end-use location, it may request the applicant to supply such information at a later stage. The applicant shall provide the information within a reasonable period of time.3.The Member State concerned shall notify the other Member States and the Commission of its intention to grant an authorisation under this Article at least ten days prior to the authorisation.

Article 4a1.It shall be prohibited to sell, supply, transfer or export, directly or indirectly, the goods and technology listed in Annex III or any other item that the Member State determines could contribute to the development of nuclear weapon delivery systems, whether or not originating in the Union, to any Iranian person, entity or body or for use in Iran.2.Annex III shall list the items, including goods and technology, contained in the Missile Technology Control Regime list.

Article 4bIt shall be prohibited:(a)to provide, directly or indirectly, technical assistance or brokering services related to the goods and technology listed in Annex III, or related to the provision, manufacture, maintenance and use of goods listed in Annex III, to any Iranian person, entity or body or for use in Iran;(b)to provide financing or financial assistance related to the goods and technology listed in Annex III, including in particular grants, loans and export credit insurance for any sale, supply, transfer or export of such items, or for any provision of related technical assistance or brokering services, directly or indirectly, to any Iranian person, entity or body, or for use in Iran;(c)to enter into any arrangement with an Iranian person, entity or body, or any person or entity acting on their behalf or at their direction, including the acceptance of loans or credit made by such person, entity or body, that would enable such person, entity or body to participate in or increase its participation, be that independently or as part of a joint venture or other partnership, in commercial activities involving technologies listed in Annex III.

Article 4cIt shall be prohibited to purchase, import or transport from Iran, directly or indirectly, the goods and technology listed in Annex III whether the item concerned originates in Iran or not.

Article 5It shall be prohibited:(a)to provide technical assistance, brokering services and other services related to the goods and technology listed in the Common Military List of the European Union ("Common Military List"), and to the provision, manufacture, maintenance and use of goods and technology on that list, directly or indirectly to any Iranian person, entity or body or for use in Iran;(b)to provide financing or financial assistance related to the goods and technology listed in the Common Military List, including in particular grants, loans and export credit insurance for any sale, supply, transfer or export of such items, or for any provision of related technical assistance or brokering services, directly or indirectly, to any Iranian person, entity or body, or for use in Iran.(c)to enter into any arrangement for the participation or increase in participation in any Iranian person, entity or body engaged in the manufacture of goods or technology listed in the Common Military List, be that independently or as part of a joint venture or other partnership. This shall include the making of loans or credit to such a person, entity or body.

Article 6Article 2(1) and Article 5(1) shall not apply to:(a)the direct or indirect transfer of goods falling within Part B of Annex I, through the territories of Member States when those goods are sold, supplied, transferred or exported to, or for use in, Iran for a light water reactor in Iran the construction of which has begun before December 2006;(b)transactions mandated by the IAEA technical cooperation programme; or(c)goods supplied or transferred to, or for use in, Iran due to obligations of State Parties under the Paris Convention on the Prohibition of the Development, Production, Stockpiling and Use of Chemical Weapons and on their Destruction of 13 January 1993 ; or(d)the execution, until 15 April 2013, of contracts concluded before 22 December 2012 for the sale, supply, transfer or export of goods and technology as specified in Part C of Annex I to this Regulation or ancillary contracts necessary for the execution of such contracts.(e)the execution, until 15 April 2013, of contracts concluded before 22 December 2012 for the provision of technical assistance or financing or financial assistance related to goods and technology as specified in Part C of Annex I to this Regulation.

Article 71.Without prejudice to Article 1(b) of Regulation (EU) No 359/2011, the competent authorities may grant, under such terms and conditions as they deem appropriate, an authorisation for a transaction in relation to goods and technology referred to in Article 2(1) of this Regulation or assistance or brokering services referred to in Article 5(1), provided that:(a)the goods and technology, assistance or brokering services are for food, agricultural, medical or other humanitarian purposes; and(b)in those cases where the transaction concerns goods or technology contained in the Nuclear Suppliers Group or Missile Technology Control Regime lists, the Sanctions Committee has determined in advance and on a case-by-case basis that the transaction would clearly not contribute to the development of technologies in support of Iran's proliferation-sensitive nuclear activities, or to the development of nuclear weapon development delivery systems.2.The Member State concerned shall inform the other Member States and the Commission, within four weeks, of authorisations granted under this Article.

Article 81.It shall be prohibited to sell, supply, transfer or export key equipment or technology listed in Annexes VI and VIA, directly or indirectly, to any Iranian person, entity or body, or for use in Iran.2.Annexes VI and VIA shall include key equipment and technology for the following key sectors of the oil and gas industry in Iran:(a)exploration of crude oil and natural gas;(b)production of crude oil and natural gas;(c)refining;(d)liquefaction of natural gas.3.Annexes VI and VIA shall also include key equipment and technology for the petrochemical industry in Iran.4.Annexes VI and VIA shall not include items included in the Common Military List, or in Annex I, II or III.

Article 9It shall be prohibited:(a)to provide, directly or indirectly, technical assistance or brokering services related to the key equipment and technology listed in Annexes VI and VIA, or related to the provision, manufacture, maintenance and use of goods listed in Annexes VI and VIA, to any Iranian person, entity or body, or for use in Iran;(b)to provide, directly or indirectly, financing or financial assistance related to the key equipment and technology listed in Annexes VI and VIA, to any Iranian person, entity or body, or for use in Iran.

Article 101.The prohibitions in Articles 8 and 9 shall not apply to:(a)the execution, until 15 April 2013, of transactions required by a trade contract concerning key equipment or technology in the exploration of crude oil and natural gas, production of crude oil and natural gas, refining, liquefaction of natural gas as listed in Annex VI concluded before 27 October 2010, or ancillary contracts necessary for the execution of such contracts, or by a contract or agreement concluded before 26 July 2010 and relating to an investment in Iran made before 26 July 2010, nor shall they prevent the execution of an obligation arising therefrom;(b)the execution, until 15 April 2013, of transactions required by a trade contract concerning key equipment or technology for the petrochemical industry as listed in Annex VI concluded before 24 March 2012, or of ancillary contracts necessary for the execution of such contracts, or by a contract or agreement concluded before 23 January 2012 and relating to an investment in Iran made before 23 January 2012, nor shall they prevent the execution of an obligation arising therefrom;(c)the execution, until 15 April 2013, of transactions required by a trade contract concerning key equipment or technology in the exploration of crude oil and natural gas, production of crude oil and natural gas, refining, liquefaction of natural gas and for the petrochemical industry as listed in Annex VIA concluded before 16 October 2012 and relating to an investment in Iran in the exploration of crude oil and natural gas, production of crude oil and natural gas, and the refining, liquefaction of natural gas made before 26 July 2010, or relating to an investment in Iran in the petrochemical industry made before 23 January 2012, nor shall they prevent the execution of an obligation arising therefrom; or(d)the provision of technical assistance intended solely for the installation of equipment or technology delivered in accordance with points (a), (b) and (c),provided that the natural or legal person, entity or body seeking to engage in such transactions, or to provide assistance to such transactions, has notified, at least 20 working days in advance, the transaction or assistance to the competent authority of the Member State in which it is established.2.Prohibitions in Articles 8 and 9 shall be without prejudice to the execution of obligations arising from contracts referred to in Article 12(1)(b) and 14(1)(b) provided that those obligations arise from service contracts or ancillary contracts necessary for their execution and provided that the execution of those obligations has been authorised in advance by the competent authority concerned and the Member State concerned has informed the other Member States and the Commission of its intention to grant an authorisation.

Article 10a1.It shall be prohibited to sell, supply, transfer or export key naval equipment or technology listed in Annex VIB, directly or indirectly, to any Iranian person, entity or body, or for use in Iran.2.Annex VIB shall include key naval equipment or technology for ship building, maintenance or refit, including equipment or technology used in the construction of oil tankers.

Article 10b1.It shall be prohibited:(a)to provide, directly or indirectly, technical assistance or brokering services related to the key equipment and technology listed in Annex VIB, or related to the provision, manufacture, maintenance and use of goods listed in Annex VIB, to any Iranian person, entity or body, or for use in Iran;(b)to provide, directly or indirectly, financing or financial assistance related to the key equipment and technology listed in Annex VIB, to any Iranian person, entity or body, or for use in Iran.

Article 10c1.The prohibitions in Articles 10a and 10b shall be without prejudice to the supply of key naval equipment and technology to a vessel which is not owned or controlled by an Iranian person, entity or body and which has been forced into a port in Iran, or into Iranian territorial waters, under force majeure.2.The prohibitions in Articles 10a and 10b shall not apply to the execution, until 15 February 2013, of contracts concluded before 22 December 2012 or ancillary contracts necessary for the execution of such contracts.

Article 10d1.A prior authorisation shall be required for:(a)the sale, supply, transfer or export of the software listed in Annex VIIA, to any Iranian person, entity or body or for use in Iran.(b)the provision of technical assistance or brokering services related to the software listed in Annex VIIA or related to the provision, manufacture, maintenance and use of such items, to any Iranian person, entity or body, or for use in Iran;(c)the provision of financing or financial assistance related to the software listed in Annex VIIA, including in particular grants, loans and export credit insurance for any sale, supply, transfer or export of such items, or for any provision of related technical assistance or brokering services to any Iranian person, entity or body, or for use in Iran.2.The competent authorities shall not grant any authorisation under this Article if:(a)they have reasonable grounds to determine that the sale, supply, transfer or export of the software is or may be intended for use in connection with the following:(i)reprocessing- or enrichment-related, heavy water-related, or other nuclear-related activities inconsistent with the JCPOA;(ii)Iran's military or ballistic missile programme; or(iii)the direct or indirect benefit of the Iranian Revolutionary Guard Corps;(b)contracts for delivery of such items or assistance do not include appropriate end-user guarantees.3.The Member State concerned shall notify the other Member States and the Commission of its intention to grant an authorisation under this Article at least ten days prior to granting the authorisation.4.Where a competent authority refuses to grant an authorisation, or annuls, suspends, substantively modifies or revokes an authorisation in accordance with this Article, the Member State concerned shall notify the other Member States, the Commission and the High Representative thereof and share the relevant information with them.5.Before a competent authority of a Member State grants an authorisation in accordance with this Article for a transaction which is essentially identical to a transaction which is the subject of a still valid denial issued by another Member State or by other Member States, it shall first consult the Member State or Member States which issued the denial. If, following such consultations, the Member State concerned decides to grant an authorisation, it shall inform the other Member States, the Commission and the High Representative thereof, providing all relevant information to explain the decision.

Article 10e1.It shall be prohibited:(a)to provide, directly or indirectly, technical assistance or brokering services related to the software listed in Annex VIIA, or related to the provision, manufacture, maintenance and use of goods listed in Annex VIIA, to any Iranian person, entity or body, or for use in Iran;(b)to provide, directly or indirectly, financing or financial assistance related to the software listed in Annex VIIA, to any Iranian person, entity or body, or for use in Iran.

Article 10f1.The prohibitions in Articles 10d and 10e shall not apply to the execution, until 15 January 2013, of contracts concluded before 22 December 2012 or ancillary contracts necessary for the execution of such contracts.

Article 111.It shall be prohibited:(a)to import crude oil or petroleum products into the Union if they:(i)originate in Iran; or(ii)have been exported from Iran;(b)to purchase crude oil or petroleum products which are located in or which originated in Iran;(c)to transport crude oil or petroleum products if they originate in Iran, or are being exported from Iran to any other country; and(d)to provide, directly or indirectly, financing or financial assistance, including financial derivatives, as well as insurance and re-insurance related to the import, purchase or transport of crude oil and petroleum products of Iranian origin or that have been imported from Iran.2.Crude oil and petroleum products means the products listed in Annex IV.3.The prohibition laid down in point (c) of paragraph 1 shall be suspended as regards the products listed in Annex XI.4.The prohibition laid down in point (d) of paragraph 1 shall be suspended insofar as it concerns the provision of insurance and reinsurance related to the import, purchase or transport of the products listed in Annex XI.

Article 121.The prohibitions in Article 11 shall not apply to:(a)the execution until 1 July 2012, of trade contracts concluded before 23 January 2012, or of ancillary contracts necessary for the execution of such contracts;(b)the execution of contracts concluded before 23 January 2012, or of ancillary contracts, necessary for the execution of such contracts, where such a contract specifically provides that the supply of Iranian crude oil and petroleum products or the proceeds derived from their supply are for the reimbursement of outstanding amounts to persons, entities or bodies under the jurisdiction of Member States;(c)crude oil or petroleum products, which had been exported from Iran prior to 23 January 2012, or where the export was made pursuant to point (a) on or prior to 1 July 2012; or where the export was made pursuant to point (b);(d)the purchase of bunker oil produced and supplied by a third country other than Iran, intended for the propulsion of the engines of vessels;(e)the purchase of bunker oil for the propulsion of the engines of a vessel which has been forced into a port in Iran, or into Iranian territorial waters, under force majeure,provided that the person, entity or body seeking to perform the contract referred to in points (a), (b) and (c) has notified, at least 20 working days in advance, the activity or transaction to the competent authority of the Member State in which it is established.2.The prohibition in Article 11(1)(d) shall not apply to the provision, until 1 July 2012, directly or indirectly, of third party liability insurance and environmental liability insurance and reinsurance.

Article 131.It shall be prohibited(a)to import petrochemical products into the Union if they:(i)originate in Iran; or(ii)have been exported from Iran;(b)to purchase petrochemical products which are located in or which originated in Iran;(c)to transport petrochemical products if they originate in Iran, or are being exported from Iran to any other country; and(d)to provide, directly or indirectly, financing or financial assistance, including financial derivatives, as well as insurance and re-insurance related to the import, purchase or transport of petrochemical products of Iranian origin or that have been imported from Iran.2.Petrochemical products means the products listed in Annex V.3.The prohibitions laid down in points (a), (b), (c) and (d) of paragraph 1 shall be suspended.

Article 141.The prohibitions in Article 13 shall not apply to:(a)the execution until 1 May 2012, of trade contracts concluded before 23 January 2012, or of ancillary contracts necessary for the execution of such contracts;(b)the execution of contracts concluded before 23 January 2012, or of ancillary contracts, including transport or insurance contracts, necessary for the execution of such contracts, where a contract specifically provides that the supply of Iranian petrochemical products or the proceeds derived from their supply are for the reimbursement of outstanding amounts to persons, entities or bodies under the jurisdiction of Member States;(c)petrochemical products which had been exported from Iran prior to 23 January 2012, or where the export was made pursuant to point (a) on or prior to 1 May 2012, or where the export was made pursuant to point (b),provided that the person, entity or body seeking to perform the contract concerned has notified, at least 20 working days in advance, the activity or transaction to the competent authority of the Member State in which it is established.2.The prohibition in Article 13(1)(d) shall not apply to the provision, until 1 May 2012, directly or indirectly, of third party liability insurance and environmental liability insurance and reinsurance.

Article 14a1.It shall be prohibited:(a)to purchase, transport, or import into the Union natural gas which originates in Iran or has been exported from Iran;(b)to swap natural gas which originates in Iran or has been exported from Iran;(c)to provide, directly or indirectly, brokering services, financing or financial assistance, including financial derivatives, as well as insurance and re-insurance and brokering services relating to insurance and re-insurance, in respect of the activities in points (a) or (b).2.The prohibitions in paragraph 1 shall not apply to:(a)natural gas that has been exported from a State other than Iran when the exported gas has been combined with gas originating from Iran within the infrastructure of a State other than Iran;(b)the purchase of natural gas within Iran by nationals of Member States for civilian purposes, including residential heating or power, or for the maintenance of diplomatic missions; or(c)the execution of contracts for the delivery of natural gas originating in a State other than Iran into the Union.3."Natural gas" means the products listed in Annex IVA.4.For the purpose of paragraph 1, "to swap" means to exchange natural gas streams of different origins.

Article 151.It shall be prohibited:(a)to sell, supply, transfer or export, directly or indirectly, gold, precious metals and diamonds, as listed in Annex VII, whether or not originating in the Union, to the Government of Iran, its public bodies, corporations and agencies, any person, entity or body acting on their behalf or at their direction, or any entity or body owned or controlled by them;(b)to purchase, import or transport, directly or indirectly, gold, precious metals and diamonds, as listed in Annex VII, whether the item concerned originates in Iran or not, from the Government of Iran, its public bodies, corporations and agencies and any person, entity or body acting on their behalf or at their direction, or any entity or body owned or controlled by them; and(c)to provide, directly or indirectly, technical assistance or brokering services, financing or financial assistance, related to the goods referred to in points (a) and (b), to the Government of Iran, its public bodies, corporations and agencies and any person, entity or body acting on their behalf or at their direction, or any enty or body owned or controlled by them.2.Annex VII shall include gold, precious metals and diamonds subject to the prohibitions referred to in paragraph 1.3.The prohibitions laid down in points (a), (b) and (c) of paragraph 1 shall be suspended as regards the products listed in Annex XII.

Article 15a1.A prior authorisation shall be required for:(a)the sale, supply, transfer or export of graphite and raw or semi-finished metals as listed in Annex VIIB, to any Iranian person, entity or body or for use in Iran;(b)the provision of technical assistance or brokering services related to graphite and raw or semi-finished metals listed in Annex VIIB or related to the provision, manufacture, maintenance and use of such items, to any Iranian person, entity or body, or for use in Iran;(c)the provision of financing or financial assistance related to graphite and raw or semi-finished metals listed in Annex VIIB, including in particular grants, loans and export credit insurance for any sale, supply, transfer or export of such items, or for any provision of related technical assistance or brokering services to any Iranian person, entity or body, or for use in Iran.2.The competent authorities shall not grant any authorisation under this Article if:(a)they have reasonable grounds to determine that the sale, supply, transfer or export of the graphite and raw or semi-finished metals is or may be intended for use in connection with the following:(i)reprocessing- or enrichment-related, heavy water-related, or other nuclear related activities inconsistent with the JCPOA;(ii)Iran's military or ballistic missile programme; or(iii)the direct or indirect benefit of the Iranian Revolutionary Guard Corps;(b)contracts for delivery of such items or assistance do not include appropriate end-user guarantees.3.The Member State concerned shall notify the other Member States and the Commission of its intention to grant an authorisation under this Article at least ten days prior to granting the authorisation.4.Where a competent authority refuses to grant an authorisation, or annuls, suspends, substantively modifies or revokes an authorisation in accordance with this Article, the Member State concerned shall notify the other Member States, the Commission and the High Representative thereof and share the relevant information with them.5.Before a competent authority of a Member State grants an authorisation in accordance with this Article for a transaction which is essentially identical to a transaction which is the subject of a still valid denial issued by another Member State or by other Member States, it shall first consult the Member State or Member States which issued the denial. If, following such consultations, the Member State concerned decides to grant an authorisation, it shall inform the other Member States, the Commission and the High Representative thereof, providing all relevant information to explain the decision.6.The provisions in paragraphs 1 to 3 shall not apply in relation to the goods listed in Annexes I, II and III or in relation to Annex I to Regulation (EC) No 428/2009.

Article 15b1.It shall be prohibited:(a)to provide, directly or indirectly, technical assistance or brokering services related to the goods as listed in Annex VIIB, or related to the provision, manufacture, maintenance and use of goods listed in Annex VIIB, to any Iranian person, entity or body, or for use in Iran;(b)to provide, directly or indirectly, financing or financial assistance related to the goods listed Annex VIIB, to any Iranian person, entity or body, or for use in Iran.2.The prohibitions in paragraph 1 shall not apply in relation to the goods listed in Annexes I, II and III.

Article 15cThe prohibitions in Article 15a shall not apply to the execution, until 15 April 2013, of contracts concluded before 22 December 2012 or ancillary contracts necessary for the execution of such contracts.

Article 16It shall be prohibited to sell, supply, transfer or export, directly or indirectly, newly printed or unissued Iranian denominated banknotes and minted coinage, to, or for the benefit of the Central Bank of Iran.

CHAPTER IIIRESTRICTIONS ON FINANCING OF CERTAIN ENTREPRISES

Article 171.The following shall be prohibited:(a)the granting of any financial loan or credit to any Iranian person, entity or body referred to in paragraph 2;(b)the acquisition or extension of a participation in any Iranian person, entity or body referred to in paragraph 2;(c)the creation of any joint venture with any Iranian person, entity or body referred to in paragraph 2.2.The prohibition in paragraph 1 shall apply to any Iranian person, entity or body engaged:(a)in the manufacture of goods or technology listed in the Common Military List or in Annex I or II;(b)in the exploration or production of crude oil and natural gas, the refining of fuels or the liquefaction of natural gas; or(c)in the petrochemical industry.3.For the purposes of paragraph 2(b) and (c) only, the following definitions shall apply:(a)'exploration of crude oil and natural gas' includes the exploration for, prospection of and management of crude oil and natural gas reserves, as well as the provision of geological services in relation to such reserves;(b)'production of crude oil and natural gas' includes bulk gas transmission services for the purpose of transit or delivery to directly interconnected grids;(c)'refining' means the processing, conditioning or preparation for the ultimately final sale of fuels.(d)'petrochemical industry' means production plants for the manufacturing of items in Annex V.4.It shall be prohibited to establish cooperation with an Iranian person, entity or body engaged in the transmission of natural gas as referred to in paragraph 3(b).5.For the purposes of paragraph 4, 'cooperation' means:(a)the sharing of investment costs in an integrated or managed supply chain for the receipt or delivery of natural gas directly from or to the territory of Iran; and(b)direct cooperation for the purpose of investing in liquefied natural gas facilities within the territory of Iran or in liquefied natural gas facilities directly connected thereto.

Article 181.The making of an investment through transactions referred to in Article 17(1) in an Iranian person, entity or body engaged in the manufacture of goods or technology listed in Annex III shall be subject to an authorisation from the competent authority concerned.2.The competent authorities shall not grant any authorisation for the transactions referred to in paragraph 1, if they have reasonable grounds to determine that the action would contribute to one of the following activities:(a)Iran's enrichment-related, reprocessing or heavy water-related activities;(b)the development of nuclear weapon delivery systems by Iran; or(c)the pursuit by Iran of activities related to other topics about which the IAEA has expressed concerns or has identified as outstanding.

Article 191.By way of derogation from Article 17(2)(a), the competent authorities may grant, under such terms and conditions as they deem appropriate, an authorisation to make an investment through transactions referred to in Article 17(1), if the following conditions are met:(a)the investment is for food, agricultural, medical or other humanitarian purposes; and(b)in those cases where the investment is made in an Iranian person, entity or body engaged in the manufacture of goods or technology contained in the Nuclear Suppliers Group and Missile Technology Control Regime lists, the Sanctions Committee has determined in advance and on a case-by-case basis that the transaction would clearly not contribute to the development of technologies in support of Iran's proliferation-sensitive nuclear activities, or to the development of nuclear weapon development delivery systems.2.The Member State concerned shall inform the other Member States and the Commission, within four weeks, of authorisations granted under this Article.

Article 20Article 17(2)(b) shall not apply to the granting of a financial loan or credit or to the acquisition or extension of a participation, if the following conditions are met:(a)the transaction is required by an agreement or contract concluded before 26 July 2010; and(b)the competent authority has been informed at least 20 working days in advance of that agreement or contract.

Article 21Article 17(2)(c) shall not apply to the granting of a financial loan or credit or to the acquisition or extension of a participation, if the following conditions are met:(a)the transaction is required by an agreement or contract concluded before 23 January 2012; and(b)the competent authority has been informed at least 20 working days in advance of that agreement or contract.

Article 22It shall be prohibited to accept or approve, by concluding an agreement or by any other means, that the granting of any financial loan or credit, or the acquisition or extension of a participation, or the creation of any joint venture be made by one or more Iranian persons, entities or bodies, in an enterprise engaged in any of the following activities:(a)uranium mining,(b)uranium enrichment and reprocessing of uranium;(c)the manufacture of goods or technology included in the Nuclear Suppliers Group or Missile Technology Control Regime lists.

CHAPTER IVFREEZING OF FUNDS AND ECONOMIC RESOURCES

Article 231.All funds and economic resources belonging to, owned, held or controlled by the persons, entities and bodies listed in Annex VIII shall be frozen. Annex VIII includes the persons, entities and bodies designated by the United Nations Security Council or by the Sanctions Committee in accordance with paragraph 12 of UNSCR 1737 (2006), paragraph 7 of UNSCR 1803 (2008) or paragraph 11, 12 or 19 of UNSCR 1929 (2010).2.All funds and economic resources belonging to, owned, held or controlled by the persons, entities and bodies listed in Annex IX shall be frozen. Annex IX shall include the natural and legal persons, entities and bodies who, in accordance with Article 20(1)(b) and (c) of Council Decision 2010/413/CFSP, have been identified as:(a)being engaged in, directly associated with, or providing support for Iran's proliferation-sensitive nuclear activities or the development of nuclear weapon delivery systems by Iran, including through involvement in the procurement of prohibited goods and technology, or being owned or controlled by such a person, entity or body, including through illicit means, or acting on their behalf or at their direction;(b)being a natural or legal person, entity or body that has evaded or violated, or assisted a listed person, entity or body to evade or violate, the provisions of this Regulation, Council Decision 2010/413/CFSP or UNSCR 1737 (2006), UNSCR 1747 (2007), UNSCR 1803 (2008) and UNSCR 1929 (2010);(c)being a member of the Islamic Revolutionary Guard Corps (IRGC) or a legal person, entity or body owned or controlled by the IRGC or by one or more of its members, or a natural or legal person, entity or body acting on their behalf, or a natural or legal person, entity or body providing insurance or other essential services to IRGC, or to entities owned or controlled by them or acting on their behalf;(d)being other persons, entities or bodies that provide support, such as material, logistical or financial support, to the Government of Iran and entities owned or controlled by them, or persons and entities associated with them;(e)being a legal person, entity or body owned or controlled by the Islamic Republic of Iran Shipping Lines (IRISL), or a natural or legal person, entity or body acting on its behalf, or a natural or legal person, entity or body providing insurance or other essential services to IRISL, or to entities owned or controlled by it or acting on its behalf.Pursuant to the obligation to freeze the funds and economic resources of IRISL and of designated entities owned or controlled by IRISL, it shall be prohibited to load and unload cargoes on and from vessels owned or chartered by IRISL or by such entities in ports of Member States.The obligation to freeze the funds and economic resources of IRISL and of designated entities owned or controlled by IRISL shall not require the impounding or detention of vessels owned by such entities or the cargoes carried by them insofar as such cargoes belong to third parties, nor does it require the detention of the crew contracted by them.3.No funds or economic resources shall be made available, directly or indirectly, to or for the benefit of the natural or legal persons, entities or bodies listed in Annexes VIII and IX or.4.Without prejudice to the derogations provided for in Articles 24, 25, 26, 27, 28, 28a, 28b and 29, it shall be prohibited to supply specialised financial messaging services, which are used to exchange financial data, to the natural or legal persons, entities or bodies listed in Annexes VIII and IX.5.Annexes VIII and IX shall include the grounds for listing of listed persons, entities and bodies, as provided by the Security Council or by the Sanctions Committee.6.Annexes VIII and IX shall also include, where available, information necessary to identify the natural or legal persons, entities and bodies concerned, as provided by the Security Council or by the Sanctions Committee. With regard to natural persons, such information may include names including aliases, date and place of birth, nationality, passport and ID card numbers, gender, adress, if known, and function or profession. With regard to legal persons, entities and bodies, such information may include names, place and date of registration, registration number and place of business. With regard to airlines and shipping companies, Annexes VIII and IX shall also include, where available, information necessary to identify each vessel or aircraft belonging to a listed company such as the original registration number or name. Annexes VIII and IX shall also include the date of designation.

Article 23a1.All funds and economic resources belonging to, owned, held or controlled by the persons, entities and bodies listed in Annex XIII shall be frozen. Annex XIII includes the natural and legal persons, entities and bodies designated by the UN Security Council in accordance with paragraph 6(c) of Annex B to UNSCR 2231 (2015).2.All funds and economic resources belonging to, owned, held or controlled by the persons, entities and bodies listed in Annex XIV shall be frozen. Annex XIV shall include the natural and legal persons, entities and bodies who, in accordance with Article 20(1)(e) of Council Decision 2010/413/CFSP, have been identified as:(a)being engaged in, directly associated with, or provided support for, Iran's proliferation-sensitive nuclear activities undertaken contrary to Iran's commitments in the JCPOA or the development of nuclear weapon delivery systems by Iran, including through the involvement in procurement of prohibited items, goods, equipment, materials and technology specified in the statement set out in Annex B to UNSCR 2231 (2015), Decision 2010/413/CFSP or the Annexes to this Regulation;(b)assisting designated persons or entities in evading or acting inconsistently with the JCPOA, UNSCR 2231 (2015), Decision 2010/413/CFSP or this Regulation;(c)acting on behalf or at the direction of designated persons or entities; or(d)being a legal person, entity or body owned or controlled by designated persons or entities.3.No funds or economic resources shall be made available, directly or indirectly, to or for the benefit of the natural or legal persons, entities or bodies listed in Annexes XIII and XIV.4.Without prejudice to the derogations provided for in Articles 24, 25, 26, 27, 28, 28a, 28b or 29, it shall be prohibited to supply specialised financial messaging services, which are used to exchange financial data, to the natural or legal persons, entities or bodies listed in Annexes XIII and XIV.5.Annexes XIII and XIV shall include the grounds for listing of listed natural or legal persons, entities or bodies.6.Annexes XIII and XIV shall also include, where available, the information necessary to identify the natural or legal persons, entities or bodies concerned. With regard to natural persons, such information may include names, including aliases, date and place of birth, nationality, passport and identity card numbers, gender, address if known, and function or profession. With regard to legal persons, entities or bodies, such information may include names, place and date of registration, registration number and place of business. Annexes XIII and XIV shall also include the date of designation.

Article 24By way of derogation from Article 23 or Article 23a, the competent authorities may authorise the release of certain frozen funds or economic resources, provided that the following conditions are met:(a)the funds or economic resources are the subject of a judicial, administrative or arbitral lien established before the date on which the person, entity or body referred to in Article 23 or Article 23a has been designated by the Sanctions Committee, the UN Security Council or the Council or of a judicial, administrative or arbitral judgment rendered prior to that date;(b)the funds or economic resources will be used exclusively to satisfy claims secured by such a lien or recognised as valid in such a judgment, within the limits set by applicable laws and regulations governing the rights of persons having such claims;(c)the lien or judgment is not for the benefit of a person, entity or body listed in Annexes VIII, IX, XIII or XIV;(d)recognising the lien or judgment is not contrary to public policy in the Member State concerned; and(e)where Article 23(1) or Article 23a(1) applies, the UN Security Council has been notified by the Member State of the lien or judgment.

Article 25By way of derogation from Article 23 or Article 23a and provided that a payment by a person, entity or body listed in Annexes VIII, IX, XIII or XIV is due under a contract or agreement that was concluded by, or an obligation that arose for the person, entity or body concerned, before the date on which that person, entity or body had been designated by the Sanctions Committee, the UN Security Council or by the Council, the competent authorities may authorise, under such conditions as they deem appropriate, the release of certain frozen funds or economic resources, provided that the following conditions are met:(a)the competent authority concerned has determined that:(i)the funds or economic resources shall be used for a payment by a person, entity or body listed in Annexes VIII, IX, XIII or XIV;(ii)the payment will not contribute to an activity prohibited under this Regulation. If the payment serves as consideration for a trade activity that has already been performed and the competent authority of another Member State had given prior confirmation that the activity was not prohibited at the time it was performed, it shall be deemed, prima facie, that the payment will not contribute to a prohibited activity; and(iii)the payment is not in breach of Article 23(3) or Article 23a(3); and(b)where Article 23(1) or Article 23a(1) applies, the Member State concerned has notified the UN Security Council of that determination and its intention to grant an authorisation, and the UN Security Council has not objected to that course of action within ten working days of notification.

Article 26By way of derogation from Article 23 or Article 23a, the competent authorities may authorise the release of certain frozen funds or economic resources, or the making available of certain funds or economic resources, under such conditions as they deem appropriate, provided that the following conditions are met:(a)the competent authority concerned has determined that the funds or economic resources concerned are:(i)necessary to satisfy the basic needs of natural or legal persons, entities or bodies listed in Annexes VIII, IX, XIII or XIV and their dependent family members of such natural persons, including payments for foodstuffs, rent or mortgage, medicines and medical treatment, taxes, insurance premiums, and public utility charges;(ii)intended exclusively for payment of reasonable professional fees and reimbursement of incurred expenses associated with the provision of legal services; or(iii)intended exclusively for payment of fees or service charges for routine holding or maintenance of frozen funds or economic resources.(b)where the authorisation concerns a person, entity or body listed in Annex XIII, the Member State concerned has notified the UN Security Council of the determination referred to in point (a) and its intention to grant an authorisation, and the UN Security Council has not objected to that course of action within five working days of notification.

Article 27By way of derogation from Article 23(2) and (3) or Article 23a(2) and (3), the competent authorities may authorise the release of certain frozen funds or economic resources or the making available of certain funds or economic resources, under such conditions as they deem appropriate, after having determined that the funds or economic resources concerned are to be paid into or from an account of a diplomatic mission or consular post or an international organisation enjoying immunities in accordance with international law, insofar as such payments are intended to be used for official purposes of the diplomatic mission or consular post or international organisation.

Article 28By way of derogation from Article 23 or Article 23a, the competent authorities may authorise the release of certain frozen funds or economic resources or the making available of certain funds or economic resources, after having determined that the funds or economic resources concerned are necessary for extraordinary expenses provided that, where the authorisation concerns a person, entity or body listed in Annex XIII, the UN Security Council has been notified of that determination by the Member State concerned and the determination has been approved by the UN Security Council.

Article 28aBy way of derogation from Article 23(2) and (3) or Article 23a(2) and (3), the competent authorities may authorise, under such conditions as they deem appropriate, the release of certain frozen funds or economic resources or the making available of certain funds or economic resources, after having determined that the funds or economic resources concerned are necessary for activities directly related to equipment referred to in paragraph 2(c), subparagraph 1 of Annex B to UNSCR 2231 (2015) for light water reactors.

Article 28bBy way of derogation from Article 23 or Article 23a, the competent authorities may authorise the release of certain frozen funds or economic resources or the making available of certain funds or economic resources, under such conditions as they deem appropriate, provided that the following conditions are met:(a)the competent authority concerned has determined that the funds or economic resources concerned are:(i)necessary for the civil nuclear cooperation projects described in Annex III of the JCPOA;(ii)necessary for activities directly related to the items specified in Articles 2a and 3a, or to any other activity required for the implementation of the JCPOA; and(b)where the authorisation concerns a person, entity or body listed in Annex XIII, the UN Security Council has been notified of that determination by the Member State concerned and the determination has been approved by the UN Security Council.

Article 291.Article 23(3) or Article 23a(3) shall not prevent the crediting of the frozen accounts by financial or credit institutions that receive funds transferred by third parties to the account of a listed person, entity or body, provided that any additions to such accounts shall also be frozen. The financial or credit institution shall inform the competent authorities about such transactions without delay.2.Provided that any such interest or other earnings and payments are frozen in accordance with Article 23(1) or (2) or Article 23a(1) or (2), Article 23(3) or Article 23a(3) shall not apply to the addition to frozen accounts of:(a)interest or other earnings on those accounts; or(b)payments due under contracts, agreements or obligations that were concluded or arose before the date on which the person, entity or body referred to in Article 23 or Article 23a has been designated by the Sanctions Committee, the UN Security Council or by the Council.

CHAPTER VRESTRICTIONS ON TRANSFERS OF FUNDS AND ON FINANCIAL SERVICES

Article 301.It shall be prohibited to transfer funds between, on the one hand, financial and credit institutions falling within the scope of this Regulation as defined in Article 49, and, on the other hand:(a)credit and financial institutions and bureaux de change domiciled in Iran;(b)branches and subsidiaries, where they fall within the scope of this Regulation, of credit and financial institutions and bureaux de change domiciled in Iran;(c)branches and subsidiaries, where they do not fall within the scope of this Regulation, of credit and financial institutions and bureaux de change domiciled in Iran; and(d)credit and financial institutions and bureaux de change that are not domiciled in Iran but are controlled by persons, entities or bodies domiciled in Iran,unless such transfers fall within the scope of paragraph 2 and have been processed in accordance with paragraph 3.2.The following transfers may be authorised in accordance with paragraph 3:(a)transfers regarding foodstuffs, healthcare, medical equipment, or for agricultural or humanitarian purposes;(b)transfers regarding personal remittances;(c)transfers in connection with a specific trade contract provided that such transfer is not prohibited under this Regulation;(d)transfers regarding diplomatic missions or consular posts or international organisations enjoying immunities in accordance with international law, insofar as such transfers are intended to be used for official purposes of the diplomatic missions or consular posts or organisations enjoying immunities in accordance with international law;(e)transfers regarding payment to satisfy claims by or against an Iranian person, entity or body, or transfers of similar nature provided that they do not contribute to the activities prohibited under this Regulation, on a case-by-case basis, if the Member State concerned has notified the other Members States and the Commission at least ten days in advance of its intention to grant an authorisation;(f)transfers necessary for the execution of the obligations arising from contracts referred to in Article 12(1)(b).3.Transfers of funds which may be authorised under paragraph 2 shall be processed as follows:(a)transfers due on transactions regarding foodstuffs, healthcare, medical equipment, or for agricultural or humanitarian purposes, below EUR 1000000 or equivalent, and transfers due on transactions regarding personal remittances, below EUR 400000 or equivalent, shall be carried out without any prior authorisation.The transfer shall be notified in advance in writing to the competent authority of the Member State concerned if equal to or above EUR 10000 or equivalent;(b)transfers due on transactions regarding foodstuffs, healthcare, medical equipment, or for agricultural or humanitarian purposes, equal to or above EUR 1000000 or equivalent, and transfers due on transactions regarding personal remittances, equal to or above EUR 400000 or equivalent, shall require prior authorisation of the competent authority of the Member State concerned pursuant to paragraph 2.Member States shall inform each other of any authorisation granted at three-monthly intervals;(c)any other transfer equal to or above EUR 100000 or equivalent shall require prior authorisation of the competent authority of the Member State concerned pursuant to paragraph 2.Member States shall inform each other of any authorisation granted at three-monthly intervals.4.Transfers of funds below EUR 10000 or equivalent shall not require any prior authorisation or notification.5.Notifications and requests for authorisations relating to the transfer of funds to an entity falling within the scope of paragraph 1(a) to (d) shall be addressed by or on behalf of the payment service provider of the payer to the competent authorities of the Member States where the payment service provider is established.Notifications and requests for authorisations relating to the transfer of funds from an entity falling within the scope of paragraph 1(a) to (d) shall be addressed by or on behalf of the payment service provider of the payee to the competent authorities of the Member States where the payment service provider is established.If the payment service provider of the payer or of the payee does not fall under the scope of this Regulation, notifications and requests for authorisation shall be addressed, in the case of a transfer to an entity falling within the scope of paragraph 1(a) to (d), by the payer, and in the case of a transfer from an entity falling within the scope of paragraph 1(a) to (d), by the payee, to the competent authorities of the Member State in which, respectively, the payer or payee is resident.6.Credit and financial institutions falling within the scope of this Regulation shall, in their activities with entities referred to in paragraph 1(a) to (d) and in order to prevent infringements of the provisions of this Regulation, conduct enhanced vigilance as follows:(a)exercise continuous vigilance over account activity, particularly through their programmes on customer due diligence;(b)require that in payment instructions all information fields which relate to the originator and beneficiary of the transaction in question be completed and if that information is not supplied, refuse the transaction;(c)maintain all records of transactions for a period of five years and make them available to national authorities on request;(d)if they have reasonable grounds to suspect that activities with credit and financial institutions may be in breach of the provisions of this Regulation, report without delay their suspicions to the financial intelligence unit (FIU) or to another competent authority designated by the Member State concerned, without prejudice to Articles 5 and 23. The FIU or such other competent authority will serve as a national centre for receiving and analysing suspicious transaction reports regarding potential breaches of this Regulation. The FIU or such other competent authority shall have access, directly or indirectly, on a timely basis to the financial, administrative and law enforcement information that it requires to properly undertake this function, including the analysis of suspicious transaction reports.

Article 30a1.Transfers of funds to and from an Iranian person, entity or body which do not fall within the scope of Article 30(1) shall be processed as follows:(a)transfers due on transactions regarding foodstuffs, healthcare, medical equipment, or for agricultural or humanitarian purposes shall be carried out without any prior authorisation.The transfer shall be notified in advance in writing to the competent authority of the Member State concerned if equal to or above EUR 10000 or equivalent;(b)any other transfer below EUR 400000 or equivalent shall be carried out without any prior authorisation.The transfer shall be notified in advance in writing to the competent authority of the Member State concerned if equal to or above EUR 10000 or equivalent;(c)any other transfer equal to or above EUR 400000 or equivalent shall require a prior authorisation of the competent authority of the Member State concerned.Member States shall inform each other of any authorisation rejected at three-monthly intervals.2.Transfers of funds below EUR 10000 or equivalent shall not require any prior authorisation or notification.3.Notifications and requests for authorisation relating to the transfer of funds shall be processed as follows:(a)in the case of electronic transfers of funds processed by credit or financial institutions:(i)notifications and requests for authorisation relating to the transfer of funds to an Iranian person, entity or body which is located outside the Union, shall be addressed by or on behalf of the payment service provider of the payer to the competent authorities of the Member State in which the payment service provider is established;(ii)notifications and requests for authorisation relating to the transfer of funds from an Iranian person, entity or body which is located outside the Union, shall be addressed by or on behalf of the payment service provider of the payee to the competent authorities of the Member State in which the payment service provider is established;(iii)if, in cases (i) and (ii), the payment service provider of the payer or of the payee does not fall under the scope of this Regulation, notifications and requests for authorisation shall be addressed, in the case of a transfer to an Iranian person, entity or body, by the payer, and in the case of a transfer from an Iranian person, entity or body by the payee to the competent authorities of the Member State in which, respectively, the payer or payee is resident;(iv)notifications and requests for authorisation relating to the transfer of funds to an Iranian person, entity or body which is located within the Union, shall be addressed by or on behalf of the payment service provider of the payee to the competent authorities of the Member States in which the payment service provider is established;(v)notifications and requests for authorisation relating to the transfer of funds from an Iranian person, entity or body which is located within the Union, shall be addressed by or on behalf of the payment service provider of the payer to the competent authorities of the Member States in which the payment service provider is established;(vi)if, in cases (iv) and (v), the payment service provider of the payer or of the payee does not fall under the scope of this Regulation, notifications and requests for authorisation shall be addressed, in the case of a transfer to an Iranian person, entity or body, by the payer, and in the case of a transfer from an Iranian person, entity or body by the payee to the competent authorities of the Member State in which, respectively, the payee or payer is resident;(vii)in relation to a transfer of funds to or from an Iranian person, entity or body where neither the payer nor the payee, nor their respective payment service providers, fall under the scope of this Regulation but a payment service provider which does fall under the scope of this Regulation acts as an intermediary, then that payment service provider must comply with the obligation to notify or seek authorisation, as applicable, if it knows or has reasonable cause to suspect that the transfer is to or from an Iranian person, entity or body. Where there is more than one payment service provider acting as an intermediary, only the first payment service provider to process the transfer is required to comply with the obligation to notify or seek authorisation, as applicable. Any notification or request for authorisation must be addressed to the competent authorities of the Member State in which the payment service provider is established;(viii)where there is more than one payment service provider involved in a series of linked transfers of funds, transfers within the Union shall include a reference to the authorisation granted under this Article;(b)in the case of transfers of funds which are made by non-electronic means, notifications and requests for authorisation relating to the transfer of funds shall be processed as follows:(i)notifications and requests for authorisation relating to transfers to an Iranian person, entity or body shall be addressed by the payer to the competent authorities of the Member State where the payer is resident;(ii)notifications and requests for authorisation relating to the transfers from an Iranian person, entity or body shall be addressed by the payee to the competent authorities of the Member State in which the payee is resident.

Article 30b1.Where an authorisation has been granted in accordance with Articles 24, 25, 26, 27, 28 or 28a, Articles 30 and 30a shall not apply.The requirement for prior authorisation of transfers of funds as provided for in Articles 30(3)(b) and (c), shall be without prejudice to the execution of transfers of funds notified to or authorised by the competent authority in advance before 22 December 2012. Such transfers of funds shall be executed before 15 April 2013.Articles 30 and 30a shall not apply with regard to transfers of funds provided for in Article 29.2.Articles 30(3) and 30a(1) shall apply regardless of whether the transfer of funds is executed in a single operation or in several operations which appear to be linked. For the purpose of this Regulation, "operations which appear to be linked" includes:(a)a series of consecutive transfers from or to the same financial or credit institutions within the scope of Article 30(1)(a) to (d) or from or to the same Iranian person, entity or body which are made in connection with a single obligation to a transfer of funds, where each individual transfer falls below the relevant threshold set out in Articles 30 and 30a but which, in the aggregate, meet the criteria for notification or authorisation; or(b)a chain of transfers involving different payment service providers or natural or legal persons which effects a single obligation to make a transfer of funds.3.For the purposes of Article 30(3)(b) and 30(3)(c) and Article 30a(1)(c), the competent authorities shall grant the authorisation, under such terms and conditions as they deem appropriate, unless they have reasonable grounds to determine that the transfer of funds for which the authorisation is requested could be in breach of any of the prohibitions or obligations in this Regulation.A competent authority may charge a fee for the assessment of requests for authorisation.4.For the purposes of Article 30a(1)(c), an authorisation shall be deemed granted if a competent authority has received a request in writing for authorisation and, within four weeks, the competent authority has not objected in writing to the transfer of funds. If the objection is raised because an investigation is pending, the competent authority shall state this and communicate its decision without delay. The competent authorities shall have access, directly or indirectly, on a timely basis to the financial, administrative and law enforcement related information necessary for carrying out the investigation.5.The following persons, entities or bodies do not fall within the scope of Articles 30 and 30a:(a)persons, entities or bodies who merely convert paper documents into electronic data and are acting under a contract with a credit institution or a financial institution;(b)persons, entities or bodies who provide credit or financial institutions solely with a message or other support system for transmitting funds; or(c)persons, entities or bodies who provide credit or financial institutions solely with clearing and settlement systems.

Article 311.Branches and subsidiaries, falling within the scope of this Regulation as defined in Article 49, of credit and financial institutions domiciled in Iran shall notify the competent authority of the Member State where they are established of all transfers of funds carried out or received by them, the names of the parties and the amount and the date of the transaction, within five working days after carrying out or receiving the transfer of funds concerned. If the information is available, the notification must specify the nature of the transaction and, where appropriate, the nature of the goods covered by the transaction and must, in particular, state whether the goods are covered by Annex I, II, III, IV, IVA, V, VI, VIA, VIB, VII, VIIA or VIIB of this Regulation and, if their export is subject to authorisation, indicate the number of the licence granted.2.Subject to and in accordance with the information-sharing arrangements, the notified competent authorities shall without delay transmit the information on notifications referred to in paragraph 1, as necessary, in order to prevent any transaction that could contribute to proliferation-sensitive nuclear activities or to the development of nuclear weapons delivery systems, to the competent authorities of other Member States where the counterparts to such transactions are established.

Article 321.Credit and financial institutions shall, in their activities with entities referred to in paragraph 2 and in order to prevent infringements of the provisions of this Regulation, conduct enhanced vigilance as follows:(a)exercise continuous vigilance over account activity, particularly through their programmes on customer due diligence;(b)require that in payment instructions all information fields which relate to the originator and beneficiary of the transaction in question be completed and if that information is not supplied, refuse the transaction;(c)maintain all records of transactions for a period of five years and make them available to national authorities on request;(d)if they have reasonable grounds to suspect that activities with credit and financial institutions may be in breach of the provisions of this Regulation, report without delay their suspicions to the financial intelligence unit (FIU) or to another competent authority designated by the Member State concerned, without prejudice to Articles 5 and 23. The FIU or such other competent authority will serve as a national centre for receiving and analysing suspicious transaction reports regarding potential breaches of this Regulation. The FIU or such other competent authority shall have access, directly or indirectly, on a timely basis to the financial, administrative and law enforcement information that it requires to properly undertake this function, including the analysis of suspicious transaction reports.2.The measures set out in paragraph 1 shall apply to credit and financial institutions in their activities with:(a)bureaux de change, credit and financial institutions domiciled in Iran;(b)branches and subsidiaries, where they fall within the scope of Article 49, of credit and financial institutions and bureaux de change domiciled in Iran;(c)branches and subsidiaries, where they do not fall within the scope of Article 49, of credit and financial institutions and bureaux de change domiciled in Iran; and(d)bureaux de change, credit and financial institutions that are not domiciled in Iran but are controlled by persons and entities domiciled in Iran.

Article 331.It shall be prohibited for credit and financial institutions falling within the scope of Article 49 to do any of the following:(a)to open a new bank account with a credit or financial institution domiciled in Iran or with any credit or financial institution referred to in Article 30(1);(b)to establish a new correspondent banking relationship with a credit or financial institution domiciled in Iran or with any credit or financial institution referred to in Article 30(1),(c)to open a new representative office in Iran or to establish a new branch or subsidiary in Iran;(d)to establish a new joint venture with a credit or financial institution domiciled in Iran or with any credit or financial institution referred to in Article 30(1).2.It shall be prohibited:(a)to authorise the opening of a representative office or the establishment of a branch or subsidiary in the Union of a credit or financial institution domiciled in Iran or of any credit or financial institution referred to in Article 30(1);(b)to conclude agreements for, or on behalf of, a credit or financial institution domiciled in Iran or for, or on behalf of, any credit or financial institution referred to in Article 30(1) pertaining to the opening of a representative office or the establishment of a branch or subsidiary in the Union;(c)to grant an authorisation for taking up and pursuing the business of credit institution or for any other business requiring prior authorisation, by a representative office, branch or subsidiary of a credit or financial institution domiciled in Iran or of any credit or financial institution referred to in Article 30(1), if the representative office, branch or subsidiary was not operational before 26 July 2010.(d)to acquire or to extend a participation, or to acquire any other ownership interest, in a credit or financial institution falling within the scope of Article 49 by any credit or financial institution referred to in Article 30(1).

Article 34It shall be prohibited:(a)to sell or purchase public or public-guaranteed bonds issued after 26 July 2010, directly or indirectly, to or from any of the following:(i)Iran or its Government, and its public bodies, corporations and agencies;(ii)a credit or financial institution domiciled in Iran or any credit or financial institution referred to in Article 30(1);(iii)a natural person or a legal person, entity or body acting on behalf or at the direction of a legal person, entity or body referred to in (i) or (ii);(iv)a legal person, entity or body owned or controlled by a person, entity or body referred to in (i), (ii) or (iii);(b)to provide brokering services with regard to public or public-guaranteed bonds issued after 26 July 2010 to a person, entity or body referred to in point (a);(c)to assist a person, entity or body referred to in point (a) in order to issue public or public-guaranteed bonds, by providing brokering services, advertising or any other service with regard to such bonds.

Article 351.It shall be prohibited to provide insurance or re-insurance, or to broker the provision of insurance or reinsurance, to:(a)Iran or its Government, and its public bodies, corporations and agencies;(b)an Iranian person, entity or body other than a natural person; or(c)a natural person or a legal person, entity or body when acting on behalf or at the direction of a legal person, entity or body referred to in (a) or (b).2.Points (a) and (b) of paragraph 1 shall not apply to the provision or brokering of compulsory or third party liability insurance or reinsurance to Iranian persons, entities and bodies based in the Union, nor to the provision of insurance for Iranian diplomatic or consular missions in the Union.3.Point (c) of paragraph 1 shall not apply to the provision of insurance or brokering of insurance, including health and travel insurance or reinsurance, to individuals acting in their private capacity, except for persons listed in Annexes VIII and IX.Point (c) of paragraph 1 shall not prevent the provision of insurance or re-insurance or brokering of insurance to the owner of a vessel, aircraft or vehicle chartered by a person, entity or body referred to in point (a) or (b) of paragraph 1.For the purpose of point (c) of paragraph 1, a person, entity or body shall not be considered to act at the direction of a person, entity or body referred to in points (a) and (b) of paragraph 1 where that direction is for the purposes of docking, loading, unloading or safe transit of a vessel or aircraft temporarily in Iranian waters or airspace.4.This Article prohibits the extension or renewal of insurance and re-insurance agreements concluded before 27 October 2010, but, without prejudice to Article 23(3), it does not prohibit compliance with agreements concluded before that date.

CHAPTER VIRESTRICTIONS ON TRANSPORT

Article 36The person providing advance information as determined in the relevant provisions concerning summary declarations as well as customs declarations in Regulation (EEC) No 2913/92 and in Regulation (EEC) No 2454/93 shall also present any authorisations if required by this Regulation.

Article 371.The provision of bunkering or ship supply services, or any other servicing of vessels, to vessels owned or controlled, directly or indirectly, by an Iranian person, entity or body shall be prohibited where the providers of the service have information, including from the competent customs authorities on the basis of the advance information referred to in Article 36, that provides reasonable grounds to determine that the vessels carry goods covered by the Common Military List or goods whose supply, sale, transfer or export is prohibited under this Regulation, unless the provision of such services is necessary for humanitarian and safety purposes.2.The provision of engineering and maintenance services to cargo aircraft owned or controlled, directly or indirectly, by an Iranian person, entity or body shall be prohibited, where the providers of the service have information, including from the competent customs authorities on the basis of the advance information referred to in Article 36, that provides reasonable grounds to determine that the cargo aircraft carry goods covered by the Common Military List or goods the supply, sale, transfer or export of which is prohibited under this Regulation, unless the provision of such services is necessary for humanitarian and safety purposes.3.The prohibitions in paragraphs 1 and 2 of this Article shall apply until the cargo has been inspected and, where necessary, seized or disposed of, as the case may be.Any seizure and disposal may, in accordance with national legislation or the decision of a competent authority, be carried out at the expense of the importer or be recovered from any other person or entity responsible for the attempted illicit supply, sale, transfer or export.

Article 37a1.The provision of the following services in respect of oil tankers and cargo vessels flying the flag of the Islamic Republic of Iran or owned, chartered, or operated, directly or indirectly, by an Iranian person, entity or body shall be prohibited:(a)the provision of classification services of any kind, including but not limited to:(i)the production and application of classification rules or technical specifications concerning the design, construction, equipment and maintenance of ships, as well as shipboard management systems;(ii)the carrying out of surveys and inspections in accordance with classification rules and procedures;(iii)the assignment of a class notation and the delivery, endorsement or renewal of certificates of compliance with classification rules or specifications;(b)the supervision of and participation in the design, construction and repair of ships and their parts including blocks, elements, machinery, electrical installations and control installation, as well as related technical assistance, financing or financial assistance;(c)the inspection, testing and certification of marine equipment, materials and components as well as the supervision of the installation on board and the supervision of system integration;(d)the carrying out of surveys, inspections, audits and visits and the issuance, renewal or endorsement of the relevant certificates and documents of compliance, on behalf of the flag State administration, in accordance with the International Convention for the Safety of Life at Sea, 1974, as amended (SOLAS 1974) and its 1988 Protocol; the International Convention for the Prevention of Pollution from Ships, 1973, as modified by the Protocol of 1978 relating thereto, as amended (MARPOL 73/78); the Convention on the International Regulations for Preventing Collisions at Sea, 1972, as amended (COLREG 1972); the International Convention on Load Lines, 1966 (LL 1966) and its 1988 Protocol; the International Convention on Standards of Training, Certification and Watchkeeping for Seafarers, 1978, as amended (STCW); and the International Convention on Tonnage Measurement of Ships, 1969 (TONNAGE 1969).2.The prohibition in paragraph 1 shall apply from 15 January 2013.

Article 37b1.It shall be prohibited to make available vessels designed for the transport or storage of oil and petrochemical products:(i)to any Iranian person, entity or body; or(ii)to any other person, entity or body, unless the providers of vessels have taken appropriate action to prevent the vessel from being used to carry or store oil or petrochemical products that originate in Iran or have been exported from Iran.2.The prohibition in paragraph 1 shall be without prejudice to the execution of obligations arising from contracts and ancillary contracts referred to in Article 12(1)(b) and (c) and in Article 14(1)(b) and (c), provided that the import and transport of Iranian crude oil, petroleum or petrochemical products have been notified to the competent authority pursuant to Article 12(1) or 14(1).3.The prohibition laid down in paragraph 1 shall be suspended.

CHAPTER VIIGENERAL AND FINAL PROVISIONS

Article 381.No claims in connection with any contract or transaction the performance of which has been affected, directly or indirectly, in whole or in part, by the measures imposed under this Regulation, including claims for indemnity or any other claim of this type, such as a claim for compensation or a claim under a guarantee, notably a claim for extension or payment of a bond, guarantee or indemnity, particularly a financial guarantee or financial indemnity, of whatever form, shall be satisfied, if they are made by:(a)designated persons, entities or bodies listed in Annexes VIII, IX, XIII and XIV;(b)any other Iranian person, entity or body, including the Iranian government;(c)any person, entity or body acting through or on behalf of one of the persons, entities or bodies referred to in points (a) and (b).2.The performance of a contract or transaction shall be regarded as having been affected by the measures imposed under this Regulation where the existence or content of the claim results directly or indirectly from those measures.3.In any proceedings for the enforcement of a claim, the onus of proving that satisfying the claim is not prohibited by paragraph 1 shall be on the person seeking the enforcement of that claim.4.This Article is without prejudice to the right of the persons, entities and bodies referred to in paragraph 1 to judicial review of the legality of the non-performance of contractual obligations in accordance with this Regulation.

Article 39For the purposes of Articles 8 and 9, point (b) of Article 17(2), and Articles 30 and 35, any body, entity or holder of rights derived from an original award before 27 October 2010 by a sovereign Government other than Iran, of a production sharing agreement shall not be considered an Iranian person, entity or body. In such cases and in relation to Article 8, the competent authority of the Member State may require appropriate end-user guarantees from any body or entity for any sale, supply, transfer or export of any key equipment or technology listed in Annex VI.

Article 401.Without prejudice to the applicable rules concerning reporting, confidentiality and professional secrecy, natural and legal persons, entities and bodies shall:(a)supply immediately any information which would facilitate compliance with this Regulation, such as information on accounts and amounts frozen in accordance with Article 23 or 23a, to the competent authorities of the Member States where they are resident or located, and shall transmit such information, directly or through the Member States, to the Commission;(b)cooperate with the competent authorities in any verification of this information.2.Any additional information received directly by the Commission shall be made available to the Member State concerned.3.Any information provided or received in accordance with this Article shall be used only for the purposes for which it was provided or received.

Article 41It shall be prohibited to participate, knowingly and intentionally, in activities the object or effect of which is to circumvent the measures in Article 2a, 2b, 2c, 2d, 3a, 3b, 3c, 3d, 4a, 4b, 5, 10d, 15a, 23, 23a and 37 of this Regulation.

Article 421.The freezing of funds and economic resources or the refusal to make funds or economic resources available, carried out in good faith on the basis that such action is in accordance with this Regulation, shall not give rise to liability of any kind on the part of the natural or legal person, entity or body implementing it, or its directors or employees, unless it is proved that the funds and economic resources were frozen or withheld as a result of negligence.2.The measures set out in the present Regulation shall not give rise to liability of any kind on the part of the natural or legal persons, entities or bodies concerned, if they did not know, and had no reasonable cause to suspect, that their actions would infringe these prohibitions.3.The disclosure in good faith, as provided for in Articles 30, 31 and 32 by a person, entity or body covered by this Regulation or an employee or director of such person, entity or body, of the information referred to in Articles 30, 31 and 32 shall not give rise to liability of any kind on the part of the institution or person or its directors or employees.

Article 431.A Member State may take all action it deems necessary to ensure that relevant international, Union or national legal obligations concerning the health and safety of workers and environmental protection are respected where cooperation with an Iranian person, entity or body may be affected by the implementation of this Regulation.2.For the purpose of action taken pursuant to paragraph 1, the prohibitions in Articles 8 and 9, point (b) of Article 17(2), and Articles 23(2), 30 and 35 shall not apply.3.The Member State concerned shall notify the other Member States and the Commission of the determination referred to in paragraph 1 and its intention to grant an authorisation at least ten working days prior to the authorisation. In case of threat to the environment and/or to the health and safety of workers in the Union requiring urgent action, the Member State concerned may grant an authorisation without prior notification and shall notify the other Member States and the Commission within three working days after having granted the authorisation.

Article 43a1.By way of derogation from Articles 8, 9, Article 17(1) as regards an Iranian person, entity or body referred to in Article 17(2)(b), Articles 23(2) and (3) insofar as they refer to persons, entities and bodies listed in Annex IX, Article 30 and 35, the competent authorities of a Member State may authorise, under such conditions as they deem appropriate, activities related to the exploration for, or exploitation of, hydrocarbons within the Union undertaken pursuant to a licence for such exploration or exploitation issued by a Member State to a person, entity or body listed in Annex IX, if the following conditions are met:(a)the licence for the exploration for, or exploitation of, hydrocarbons within the Union was issued prior to the date on which the person, entity or body listed in Annex IX was designated; and(b)the authorisation is necessary to avoid or remediate environmental damage in the Union or to prevent permanent destruction of the licence's value, including by securing the pipeline and infrastructure used in connection with the licensed activity, on a temporary basis. Such authorisation may include measures taken under national legislation.2.The derogation provided for in paragraph 1 shall only be granted for such period as necessary and its validity shall not exceed the validity of the licence issued to the person, entity or body listed in Annex IX. In case the competent authority considers that subrogation to contracts or the provision of indemnities is necessary, the period of validity of the derogation shall not exceed five years.3.The Member State concerned shall notify the other Member States and the Commission of its intention to grant an authorisation at least ten working days prior to the authorisation. In case of threat to the environment in the Union requiring urgent action to prevent damage to the environment, the Member State concerned may grant an authorisation without prior notification and shall notify the other Member States and the Commission within three working days after having granted the authorisation.

Article 43b1.Notwithstanding other provisions of this Regulation, the competent authorities may authorise the supply, sale, or transfer of items, materials, equipment, goods and technology, and the provision of any related technical assistance, training, financial assistance, investment, brokering or other services where they consider them to be directly related to:(a)the modification of two cascades at the Fordow facility for stable isotope production;(b)the export of Iran's enriched uranium in excess of 300 kilograms in return for natural uranium; or(c)the modernisation of the Arak reactor based on the agreed conceptual design and, subsequently, on the agreed final design of such reactor.2.The competent authority granting an authorisation in accordance with paragraph 1 shall ensure that:(a)all activities are undertaken strictly in accordance with the Joint Comprehensive Plan of Action of 14 July 2015 ("JCPOA");(b)the requirements, as appropriate, specified in subparagraph 22(c) of UNSCR 2231 (2015) have been met; and(c)it has obtained and is in a position to exercise effectively a right to verify the end-use and end-use location of any supplied item.3.The Member State concerned shall notify:(a)the Sanctions Committee and, when constituted, the Joint Commission, as appropriate, 10 days before granting the authorisation;(b)the IAEA within 10 days of the supply, sale or transfer, in the case of supplied items, materials, equipment, goods and technology specified in subparagraph 22(e) of UNSCR 2231 (2015).4.The Member State concerned shall notify the other Member States and the Commission of its intention to grant an authorisation under this Article at least 10 days prior to the authorisation.

Article 43c1.Notwithstanding other provisions of this Regulation, the competent authorities may authorise, on a case-by-case basis, transfers and activities, in so far as necessary for their execution, that are:(a)directly related to the implementation of the nuclear-related actions specified in paragraphs 15.1 to 15.11 of Annex V to the JCPOA;(b)required for preparation for the implementation of the JCPOA; or(c)determined by the Sanctions Committee, as appropriate, to be consistent with the objectives of UNSCR 2231 (2015).2.The Member State concerned shall, as appropriate, submit the proposed authorisations to the Sanctions Committee for approval.3.The Member State concerned shall notify the other Member States and the Commission of its intention to grant an authorisation under this Article at least 10 days prior to the authorisation.

Article 441.The Commission and Member States shall inform each other of the measures taken under this Regulation and share any other relevant information at their disposal in connection with this Regulation at three-monthly intervals, in particular information(a)in respect of funds frozen under Articles 23 and 23a and authorisations granted under Articles 24, 25, 26, 27, 28, 28a and 28b;(b)in respect of violations and enforcement problems and judgments issued by national courts.2.The Member States shall immediately inform each other and the Commission of any other relevant information at their disposal which might affect the effective implementation of this Regulation.

Article 45The Commission shall amend Annexes I, II, III, VIIA, VIIB and X on the basis of information supplied by Member States.

Article 461.Where the UN Security Council lists a natural or legal person, entity or body, the Council shall include such natural or legal person, entity or body in Annex VIII.2.Where the Council decides to subject a natural or legal person, entity or body to the measures referred to in Article 23(2) and (3), it shall amend Annex IX accordingly.3.Where the Council decides to subject a natural or legal person, entity or body to the measures referred to in Article 23a(2) and (3), it shall amend Annex XIV accordingly.4.The Council shall communicate its decision, including the grounds for listing, to the natural or legal person, entity or body referred to in paragraphs 1 to 3, either directly, if the address is known, or through the publication of a notice, providing such natural or legal person, entity or body with an opportunity to present observations.5.Where observations are submitted, or where substantial new evidence is presented, the Council shall review its decision and inform the natural or legal person, entity or body accordingly.6.Where the United Nations decides to delist a natural or legal person, entity or body, or to amend the identifying data of a listed natural or legal person, entity or body, the Council shall amend Annex VIII or XIII accordingly.7.The lists in Annexes IX and XIV shall be reviewed in regular intervals and at least every 12 months.

Article 471.Member States shall lay down the rules on penalties applicable to infringements of this Regulation and shall take all measures necessary to ensure that they are implemented. The penalties provided for shall be effective, proportionate and dissuasive.2.Member States shall notify the Commission of those rules without delay after the entry into force of this Regulation and shall notify it of any subsequent amendment.

Article 481.Member States shall designate the competent authorities referred to in this Regulation and identify them on the websites listed in Annex X. Member States shall notify the Commission of any changes in the addresses of their websites listed in Annex X.2.Member States shall notify the Commission of their competent authorities, including the contact details of those competent authorities, without delay after the entry into force of this Regulation, and shall notify it of any subsequent amendment.3.Where this Regulation sets out a requirement to notify, inform or otherwise communicate with the Commission, the address and other contact details to be used for such communication shall be those indicated in Annex X.

Article 49This Regulation shall apply:(a)within the territory of the Union, including its airspace;(b)on board any aircraft or any vessel under the jurisdiction of a Member State;(c)to any person inside or outside the territory of the Union who is a national of a Member State;(d)to any legal person, entity or body, inside or outside the territory of the Union, which is incorporated or constituted under the law of a Member State;(e)to any legal person, entity or body in respect of any business done in whole or in part within the Union.

Article 50Regulation (EU) No 961/2010 is hereby repealed. References to the repealed regulation shall be construed as references to this Regulation.

Article 51This Regulation shall enter into force on the day of its publication in the Official Journal of the European Union.

This Regulation shall be binding in its entirety and directly applicable in all Member States.ANNEX ICATEGORY 0 — NUCLEAR MATERIALS, FACILITIES, AND EQUIPMENT0ASystems, Equipment and Components

Item codes marked with a "TLB" refer to items listed in Annex B of the NSG Part 1 Trigger List. Item codes marked with "TLA" refer to items listed in Annex A of NSG Part 1 Trigger List. Item codes marked with neither "TLB" nor "TLA" refer to items listed in the NSG Dual Use List, referenced in the Categories 1, 2 and 6.

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.12/Part 1
0A001	"Nuclear reactors" and specially designed or prepared equipment and components therefor, as follows:	TLB1.1	Complete nuclear reactors
0A001.a	"Nuclear reactors";	TLB1.1	Nuclear reactors capable of operation so as to maintain a controlled self-sustaining fission chain reaction.EXPLANATORY NOTE A "nuclear reactor" basically includes the items within or attached directly to the reactor vessel, the equipment which controls the level of power in the core, and the components which normally contain or come in direct contact with or control the primary coolant of the reactor core. EXPORTS The export of the whole set of major items within this boundary will take place only in accordance with the procedures of the Guidelines. Those individual items within this functionally defined boundary which will be exported only in accordance with the procedures of the Guidelines are listed in paragraphs 1.2. to 1.11. The Government reserves to itself the right to apply the procedures of the Guidelines to other items within the functionally defined boundary
0A001.b	Metal vessels, or major shop-fabricated parts therefor, including the reactor vessel head for a reactor pressure vessel, specially designed or prepared to contain the core of a "nuclear reactor";	TLB1.2	Nuclear reactor vesselsMetal vessels, or major shop-fabricated parts therefor, especially designed or prepared to contain the core of a nuclear reactor as defined in paragraph 1.1. above, as well as relevant reactor internals as defined in paragraph 1.8. below.EXPLANATORY NOTE Item 1.2 covers nuclear reactor vessels regardless of pressure rating and includes reactor pressure vessels and calandrias. The reactor vessel head is covered by item 1.2. as a major shop-fabricated part of a reactor vessel.
0A001.c	Manipulative equipment specially designed or prepared for inserting or removing fuel in a "nuclear reactor";	TLB1.3	Nuclear reactor fuel charging and discharging machinesManipulative equipment especially designed or prepared for inserting or removing fuel in a nuclear reactor as defined in paragraph 1.1. above.EXPLANATORY NOTE The items noted above are capable of on-load operation or at employing technically sophisticated positioning or alignment features to allow complex off-load fueling operations such as those in which direct viewing of or access to the fuel is not normally available.
0A001.d	Control rods specially designed or prepared for the control of the fission process in a "nuclear reactor", support or suspension structures therefor, rod drive mechanisms and rod guide tubes;	TLB1.4	Nuclear reactor control rods and equipmentEspecially designed or prepared rods, support or suspension structures therefor, rod drive mechanisms or rod guide tubes to control the fission process in a nuclear reactor as defined in paragraph 1.1. above.
0A001.e	Pressure tubes specially designed or prepared to contain both fuel elements and the primary coolant in a "nuclear reactor";	TLB1.5	Nuclear reactor pressure tubesTubes which are especially designed or prepared to contain both fuel elements and the primary coolant in a reactor as defined in paragraph 1.1. above.EXPLANATORY NOTE Pressure tubes are parts of fuel channels designed to operate at elevated pressure, sometimes in excess of 5 MPa.
0A001.f	Zirconium metal tubes or zirconium alloy tubes (or assembles of tubes) specially designed or prepared for use as fuel cladding in a "nuclear reactor", and in quantities exceeding 10 kg;N.B.:For zirconium pressure tubes see 0A001.e. and for calandria tubes see 0A001.h.	TLB1.6	Nuclear fuel claddingZirconium metal tubes or zirconium alloy tubes (or assemblies of tubes) especially designed or prepared for use as fuel cladding in a reactor as defined in paragraph 1.1. above, and in quantities exceeding 10 kg.N.B.:For zirconium pressure tubes see 1.5. For calandria tubes see 1.8.EXPLANATORY NOTE Zirconium metal tubes or zirconium alloy tubes for use in a nuclear reactor consist of zirconium in which the relation of hafnium to zirconium is typically less than 1:500 parts by weight
0A001.g	Coolant pumps or circulators specially designed or prepared for circulating the primary coolant of "nuclear reactors";	TLB1.7	Primary coolant pumps or circulatorsPumps or circulators especially designed or prepared for circulating the primary coolant for nuclear reactors as defined in paragraph 1.1. above.EXPLANATORY NOTE: Especially designed or prepared pumps or circulators include pumps for water-cooled reactors, circulators for gas-cooled reactors, and electromagnetic and mechanical pumps for liquid-metal-cooled reactors. This equipment may include pumps with elaborate sealed or multi-sealed systems to prevent leakage of primary coolant, canned-driven pumps, and pumps with inertial mass systems. This definition encompasses pumps certified to Section III, Division I, Subsection NB (Class 1 components) of the American Society of Mechanical Engineers (ASME) Code, or equivalent standards.
0A001.h	"Nuclear reactor internals" specially designed or prepared for use in a "nuclear reactor", including support columns for the core, fuel channels, calandria tubes, thermal shields, baffles, core grid plates, and diffuser plates;Technical Note:In 0A001.h. "nuclear reactor internals" means any major structure within a reactor vessel which has one or more functions such as supporting the core, maintaining fuel alignment, directing primary coolant flow, providing radiation shields for the reactor vessel, and guiding in-core instrumentation.	TLB1.8	Nuclear reactor internals"Nuclear reactor internals" especially designed or prepared for use in a nuclear reactor as defined in paragraph 1.1 above. This includes, for example, support columns for the core, fuel channels, calandria tubes, thermal shields, baffles, core grid plates, and diffuser plates.EXPLANATORY NOTE "Nuclear reactor internals" are major structures within a reactor vessel which have one or more functions such as supporting the core, maintaining fuel alignment, directing primary coolant flow, providing radiation shields for the reactor vessel, and guiding in-core instrumentation.
0A001.i	Heat exchangers as follows:1.Steam generators specially designed or prepared for the primary, or intermediate, coolant circuit of a "nuclear reactor";2.Other heat exchangers specially designed or prepared for use in the primary coolant circuit of a "nuclear reactor";Note:0A001.i. does not control heat exchangers for the supporting systems of the reactor, e.g., the emergency cooling system or the decay heat cooling system.	TLB1.9	Heat exchangers(a) Steam generators especially designed or prepared for the primary, or intermediate, coolant circuit of a nuclear reactor as defined in paragraph 1.1 above. (b) Other heat exchangers especially designed or prepared for use in the primary coolant circuit of a nuclear reactor as defined in paragraph 1.1 above.EXPLANATORY NOTE Steam generators are especially designed or prepared to transfer the heat generated in the reactor to the feed water for steam generation. In the case of a fast reactor for which an intermediate coolant loop is also present, the steam generator is in the intermediate circuit. In a gas-cooled reactor, a heat exchanger may be utilized to transfer heat to a secondary gas loop that drives a gas turbine. The scope of control for this entry does not include heat exchangers for the supporting systems of the reactor, e.g., the emergency cooling system or the decay heat cooling system.
0A001.j	Neutron detectors specially designed or prepared for determining neutron flux levels within the core of a "nuclear reactor";	TLB1.10	Neutron detectorsEspecially designed or prepared neutron detectors for determining neutron flux levels within the core of a reactor as defined in paragraph 1.1. above.EXPLANATORY NOTE The scope of this entry encompasses in-core and ex-core detectors which measure flux levels in a large range, typically from 104 neutrons per cm2 per second to 1010 neutrons per cm2 per second or more. Ex-core refers to those instruments outside the core of a reactor as defined in paragraph 1.1. above, but located within the biological shielding.
0A001.k	"External thermal shields" specially designed or prepared for use in a "nuclear reactor" for the reduction of heat loss and also for the containment vessel protection.Technical Note:In 0A001.k. "external thermal shields" means major structures placed over the reactor vessel which reduce heat loss from the reactor and reduce temperature within the containment vessel.	TLB1.11	External thermal shields"External thermal shields" especially designed or prepared for use in a nuclear reactor as defined in paragraph 1.1 for reduction of heat loss and also for containment vessel protection.EXPLANATORY NOTE "External thermal shields" are major structures placed over the reactor vessel which reduce heat loss from the reactor and reduce temperature within the containment vessel.
0B001	Plant for the separation of isotopes of "natural uranium", "depleted uranium" or "special fissile materials", and specially designed or prepared equipment and components therefor, as follows:	TLB5	Plants for the separation of isotopes of natural uranium, depleted uranium or special fissionable material and equipment, other than analytical instruments, especially designed or prepared therefor
0B001.a	Plant specially designed for separating isotopes of "natural uranium", "depleted uranium", or "special fissile materials", as follows:1.Gas centrifuge separation plant;2.Gaseous diffusion separation plant;3.Aerodynamic separation plant;4.Chemical exchange separation plant;5.Ion-exchange separation plant;6.Atomic vapour "laser" isotope separation plant;7.Molecular "laser" isotope separation plant;8.Plasma separation plant;9.Electro magnetic separation plant;	TLB5
0B001.b	Gas centrifuges and assemblies and components, specially designed or prepared for gas centrifuge separation process, as follows:Technical Note:In 0B001.b. "high strength-to-density ratio material" means any of the following:1.Maraging steel capable of an ultimate tensile strength of 1,95 GPa or more;2.Aluminium alloys capable of an ultimate tensile strength of 0,46 GPa or more; or3."Fibrous or filamentary materials" with a "specific modulus" of more than 3,18 × 106 m and a "specific tensile strength" greater than 7,62 × 104 m;1.Gas centrifuges;	TLB5.1	5.1.Gas centrifuges and assemblies and components especially designed or prepared for use in gas centrifugesINTRODUCTORY NOTEThe gas centrifuge normally consists of a thin-walled cylinder(s) of between 75 mm and 650 mm diameter contained in a vacuum environment and spun at high peripheral speed of the order of 300 m/s or more with its central axis vertical. In order to achieve high speed the materials of construction for the rotating components have to be of a high strength to density ratio and the rotor assembly, and hence its individual components, have to be manufactured to very close tolerances in order to minimize the unbalance. In contrast to other centrifuges, the gas centrifuge for uranium enrichment is characterized by having within the rotor chamber a rotating disc-shaped baffle(s) and a stationary tube arrangement for feeding and extracting the UF6 gas and featuring at least three separate channels, of which two are connected to scoops extending from the rotor axis towards the periphery of the rotor chamber. Also contained within the vacuum environment are a number of critical items which do not rotate and which although they are especially designed are not difficult to fabricate nor are they fabricated out of unique materials. A centrifuge facility however requires a large number of these components, so that quantities can provide an important indication of end use.
0B001.b		TLB5.1.1	Rotating components
0B001.b.	2.Complete rotor assemblies;	TLB5.1.1a	(a)Complete rotor assemblies:Thin-walled cylinders, or a number of interconnected thin-walled cylinders, manufactured from one or more of the high strength to density ratio materials described in the EXPLANATORY NOTE to this Section. If interconnected, the cylinders are joined together by flexible bellows or rings as described in section 5.1.1.(c) following. The rotor is fitted with an internal baffle(s) and end caps, as described in section 5.1.1.(d) and (e) following, if in final form. However the complete assembly may be delivered only partly assembled.
0B001.b.	3.Rotor tube cylinders with a wall thickness of 12 mm or less, a diameter of between 75 mm and 650 mm, made from "high strength-to-density ratio materials";	TLB5.1.1b	(b)Rotor tubes:Especially designed or prepared thin-walled cylinders with thickness of 12 mm or less, a diameter of between 75 mm and 650 mm, and manufactured from one or more of the high strength to density ratio materials described in the EXPLANATORY NOTE to this Section.
0B001.b.	4.Rings or bellows with a wall thickness of 3 mm or less and a diameter of between 75 mm and 650 mm and designed to give local support to a rotor tube or to join a number together, made from "high strength-to-density ratio materials";	TLB5.1.1c	(c)Rings or Bellows:Components especially designed or prepared to give localized support to the rotor tube or to join together a number of rotor tubes. The bellows is a short cylinder of wall thickness 3 mm or less, a diameter of between 75 mm and 650 mm, having a convolute, and manufactured from one of the high strength to density ratio materials described in the EXPLANATORY NOTE to this Section.
0B001.b.	5.Baffles of between 75 mm and 650 mm diameter for mounting inside a rotor tube, made from "high strength-to-density ratio materials".	TLB5.1.1d	(d)Baffles:Disc-shaped components of between 75 mm and 650 mm diameter especially designed or prepared to be mounted inside the centrifuge rotor tube, in order to isolate the take-off chamber from the main separation chamber and, in some cases, to assist the UF6 gas circulation within the main separation chamber of the rotor tube, and manufactured from one of the high strength to density ratio materials described in the EXPLANATORY NOTE to this Section.
0B001.b.	6.Top or bottom caps of between 75 mm and 650 mm diameter to fit the ends of a rotor tube, made from "high strength-to-density ratio materials";	TLB5.1.1e	(e)Top caps/Bottom caps:Disc-shaped components of between 75 mm and 650 mm diameter especially designed or prepared to fit to the ends of the rotor tube, and so contain the UF6 within the rotor tube, and in some cases to support, retain or contain as an integrated part an element of the upper bearing (top cap) or to carry the rotating elements of the motor and lower bearing (bottom cap), and manufactured from one of the high strength to density ratio materials described in the EXPLANATORY NOTE to this Section.
		TLB5.1.1	EXPLANATORY NOTEThe materials used for centrifuge rotating components include the following:(a)Maraging steel capable of an ultimate tensile strength of 1,95 GPa or more;(b)Aluminium alloys capable of an ultimate tensile strength of 0,46 GPa or more;(c)Filamentary materials suitable for use in composite structures and having a specific modulus of 3,18 × 106 m or greater and a specific ultimate tensile strength of 7,62 × 104 m or greater ("Specific Modulus" is the Young's Modulus in N/m2 divided by the specific weight in N/m3; "Specific Ultimate Tensile Strength" is the ultimate tensile strength in N/m2 divided by the specific weight in N/m3).
0B001.b		TLB5.1.2	Static components
0B001.b.	7.Magnetic suspension bearings as follows:a.Bearing assemblies consisting of an annular magnet suspended within a housing made of or protected by "materials resistant to corrosion by UF6" containing a damping medium and having the magnet coupling with a pole piece or second magnet fitted to the top cap of the rotor;b.Active magnetic bearings specially designed or prepared for use with gas centrifuges.	TLB5.1.2A.1	(a)Magnetic suspension bearings:1.Especially designed or prepared bearing assemblies consisting of an annular magnet suspended within a housing containing a damping medium. The housing will be manufactured from a UF6-resistant material (see EXPLANATORY NOTE to Section 5.2.). The magnet couples with a pole piece or a second magnet fitted to the top cap described in Section 5.1.1.(e).The magnet may be ring-shaped with a relation between outer and inner diameter smaller or equal to 1,6:1. The magnet may be in a form having an initial permeability of 0,15 H/m or more, or a remanence of 98,5 % or more, or an energy product of greater than 80 kJ/m3. In addition to the usual material properties, it is a prerequisite that the deviation of the magnetic axes from the geometrical axes is limited to very small tolerances (lower than 0,1 mm) or that homogeneity of the material of the magnet is specially called for.
0B001.b.		TLB5.1.2a2	2.Active magnetic bearings especially designed or prepared for use with gas centrifuges.EXPLANATORY NOTEThese bearings usually have the following characteristics:Designed to keep centred a rotor spinning at 600 Hz or more, andAssociated to a reliable electrical power supply and/or to an uninterruptible power supply (UPS) unit in order to function for more than one hour.
0B001.b.	8.Specially prepared bearings comprising a pivot-cup assembly mounted on a damper;	TLB5.1.2b	(b)Bearings/Dampers:Especially designed or prepared bearings comprising a pivot/cup assembly mounted on a damper. The pivot is normally a hardened steel shaft with a hemisphere at one end with a means of attachment to the bottom cap described in section 5.1.1.(e) at the other. The shaft may however have a hydrodynamic bearing attached. The cup is pellet-shaped with a hemispherical indentation in one surface.These components are often supplied separately to the damper.
0B001.b.	9.Molecular pumps comprised of cylinders having internally machined or extruded helical grooves and internally machined bores;	TLB5.1.2c	(c)Molecular pumps:Especially designed or prepared cylinders having internally machined or extruded helical grooves and internally machined bores. Typical dimensions are as follows:75 mm to 650 mm internal diameter, 10 mm or more wall thickness, with the length equal to or greater than the diameter. The grooves are typically rectangular in cross-section and 2 mm or more in depth.
0B001.b.	10.Ring-shaped motor stators for multiphase AC hysteresis (or reluctance) motors for synchronous operation within a vacuum at a frequency of 600 Hz or more and a power of 40 VA or more;	TLB5.1.2d	(d)Motor stators:Especially designed or prepared ring-shaped stators for high speed multiphase AC hysteresis (or reluctance) motors for synchronous operation within a vacuum at a frequency of 600 Hz or greater and a power of 40 VA or greater. The stators may consist of multi-phase windings on a laminated low loss iron core comprised of thin layers typically 2,0 mm thick or less.
0B001.b.	11.Centrifuge housing/recipients to contain the rotor tube assembly of a gas centrifuge, consisting of a rigid cylinder of wall thickness up to 30 mm with precision machined ends that are parallel to each other and perpendicular to the cylinder's longitudinal axis to within 0,05 degrees or less;	TLB5.1.2e	(e)Centrifuge housing/recipients:Components especially designed or prepared to contain the rotor tube assembly of a gas centrifuge. The housing consists of a rigid cylinder of wall thickness up to 30 mm with precision machined ends to locate the bearings and with one or more flanges for mounting. The machined ends are parallel to each other and perpendicular to the cylinder's longitudinal axis to within 0,05 degrees or less. The housing may also be a honeycomb type structure to accommodate several rotor assemblies.
0B001.b.	12.Scoops consisting of specially designed or prepared tubes for the extraction of UF6 gas from within the rotor tube by a Pitot tube action and capable of being fixed to the central gas extraction system;	TLB5.1.2f	(f)Scoops:Especially designed or prepared tubes for the extraction of UF6 gas from within the rotor tube by a Pitot tube action (that is, with an aperture facing into the circumferential gas flow within the rotor tube, for example by bending the end of a radially disposed tube) and capable of being fixed to the central gas extraction system.
0B001.b.	13.Frequency changers (converters or inverters) specially designed or prepared to supply motor stators for gas centrifuge enrichment, having all of the following characteristics, and specially designed components therefor:a.A multiphase frequency output of 600 Hz or greater; andb.High stability (with frequency control better than 0,2 %);	TLB5.2.5	5.2.5.Frequency changersFrequency changers (also known as converters or inverters) especially designed or prepared to supply motor stators as defined under 5.1.2.(d), or parts, components and sub-assemblies of such frequency changers having all of the following characteristics:1.A multiphase frequency output of 600 Hz or greater; and2.High stability (with frequency control better than 0,2 %).
0B001.b.	14.Shut-off and control valves as follows:a.Shut-off valves specially designed or prepared to act on the feed, product or tails UF6 gaseous streams of an individual gas centrifuge;b.Bellows-sealed valves, shut-off or control, made of or protected by "materials resistant to corrosion by UF6", with an inside diameter of 10 mm to 160 mm, specially designed or prepared for use in main or auxiliary systems of gas centrifuge enrichment plants;	TLB5.2.3	5.2.3Special shut-off and control valves(a)Shut-off valves especially designed or prepared to act on the feed, product or tails UF6 gaseous streams of an individual gas centrifuge.(b)Bellows-sealed valves, manual or automated, shut-off or control, made of or protected by materials resistant to corrosion by UF6, with an inside diameter of 10 to 160 mm, especially designed or prepared for use in main or auxiliary systems of gas centrifuge enrichment plants.EXPLANATORY NOTETypical especially designed or prepared valves include bellow-sealed valves, fast acting closure-types, fast acting valves and others.
0B001.c	Equipment and components, specially designed or prepared for gaseous diffusion separation process, as follows:1.Gaseous diffusion barriers made of porous metallic, polymer or ceramic "materials resistant to corrosion by UF6" with a pore size of 10 to 100 nm, a thickness of 5 mm or less, and, for tubular forms, a diameter of 25 mm or less;	TLB5.3.1a	Gaseous diffusion barriers and barrier materials(a)Especially designed or prepared thin, porous filters, with a pore size of 10 — 100 nm, a thickness of 5 mm or less, and for tubular forms, a diameter of 25 mm or less, made of metallic, polymer or ceramic materials resistant to corrosion by UF6 (see EXPLANATORY NOTE to section 5.4), and
0B001.c	2.Gaseous diffuser housings made of or protected by "materials resistant to corrosion by UF6";	TLB5.3.2	Diffuser housingsEspecially designed or prepared hermetically sealed vessels for containing the gaseous diffusion barrier, made of or protected by UF6-resistant materials (see EXPLANATORY NOTE to section 5.4).
0B001.c	3.Compressors or gas blowers with a suction volume capacity of 1 m3/min or more of UF6, discharge pressure up to 500 kPa and having a pressure ratio of 10:1 or less, and made of or protected by "materials resistant to corrosion by UF6";	TLB5.3.3	Compressors and gas blowersEspecially designed or prepared compressors or gas blowers with a suction volume capacity of 1 m3 per minute or more of UF6, and with a discharge pressure of up to 500 kPa, designed for long-term operation in the UF6 environment, as well as separate assemblies of such compressors and gas blowers. These compressors and gas blowers have a pressure ratio of 10:1 or less and are made of, or protected by, materials resistant to UF6 (see EXPLANATORY NOTE to section 5.4).
0B001.c	4.Rotary shaft seals for compressors or blowers specified in 0B001.c.3. and designed for a buffer gas in-leakage rate of less than 1000 cm3/min.;	TLB5.3.4	Rotary shaft sealsEspecially designed or prepared vacuum seals, with seal feed and seal exhaust connections, for sealing the shaft connecting the compressor or the gas blower rotor with the driver motor so as to ensure a reliable seal against in-leaking of air into the inner chamber of the compressor or gas blower which is filled with UF6. Such seals are normally designed for a buffer gas in-leakage rate of less than 1000 cm3 per minute.
0B001.c	5.Heat exchangers made of or protected by "materials resistant to corrosion by UF6", and designed for a leakage pressure rate of less than 10 Pa per hour under a pressure differential of 100 kPa	TLB5.3.5	Heat exchangers for cooling UF6Especially designed or prepared heat exchangers made of or protected by UF6-resistant materials (see EXPLANATORY NOTE to section 5.4), and intended for a leakage pressure change rate of less than 10 Pa per hour under a pressure difference of 100 kPa.
0B001.c	6.Bellows-sealed valves, manual or automated, shut-off or control, made of or protected by "materials resistant to corrosion by UF6";	TLB5.4.4	Special shut-off and control valvesEspecially designed or prepared bellows-sealed valves, manual or automated, shut-off or control, made of or protected by materials resistant to corrosion by UF6, for installation in main and auxiliary systems of gaseous diffusion enrichment plants.
0B001.d	Equipment and components, specially designed or prepared for aerodynamic separation process, as follows:1.Separation nozzles consisting of slit-shaped, curved channels having a radius of curvature less than 1 mm, resistant to corrosion by UF6, and having a knife-edge contained within the nozzle which separates the gas flowing through the nozzle into two streams;	TLB5.5.1	Separation nozzlesEspecially designed or prepared separation nozzles and assemblies thereof. The separation nozzles consist of slit-shaped, curved channels having a radius of curvature less than 1 mm, resistant to corrosion by UF6 and having a knife-edge within the nozzle that separates the gas flowing through the nozzle into two fractions.
0B001.d	2.Cylindrical or conical tubes, (vortex tubes), made of or protected by "materials resistant to corrosion by UF6" and with one or more tangential inlets;	TLB5.5.2	Vortex tubesEspecially designed or prepared vortex tubes and assemblies thereof. The vortex tubes are cylindrical or tapered, made of or protected by materials resistant to corrosion by UF6, and with one or more tangential inlets. The tubes may be equipped with nozzletype appendages at either or both ends.EXPLANATORY NOTE The feed gas enters the vortex tube tangentially at one end or through swirl vanes or at numerous tangential positions along the periphery of the tube.
0B001.d	3.Compressors or gas blowers made of or protected by "materials resistant to corrosion by UF6", and rotary shaft seals therefor;	TLB5.5.3TLB5.5.4	Compressors and gas blowersEspecially designed or prepared compressors or gas blowers made of or protected by materials resistant to corrosion by the UF6/carrier gas (hydrogen or helium) mixture.Rotary shaft sealsEspecially designed or prepared rotary shaft seals, with seal feed and seal exhaust connections, for sealing the shaft connecting the compressor rotor or the gas blower rotor with the driver motor so as to ensure a reliable seal against out-leakage of process gas or in-leakage of air or seal gas into the inner chamber of the compressor or gas blower which is filled with a UF6/carrier gas mixture.
0B001.d	4.Heat exchangers made of or protected by "materials resistant to corrosion by UF6";	TLB5.5.5	Heat exchangers for gas coolingEspecially designed or prepared heat exchangers made of or protected by materials resistant to corrosion by UF6.
0B001.d	5.Separation element housings, made of or protected by "materials resistant to corrosion by UF6" to contain vortex tubes or separation nozzles;	TLB5.5.6	Separation element housingsEspecially designed or prepared separation element housings, made of or protected by materials resistant to corrosion by UF6, for containing vortex tubes or separation nozzles.
0B001.d	6.Bellows-sealed valves, manual or automated, shut-off or control, made of or protected by "materials resistant to corrosion by UF6", with a diameter of 40 mm or more;	TLB5.5.10	UF6 mass spectrometers/Ion sourcesEspecially designed or prepared mass spectrometers capable of taking on-line samples from UF6 gas streams and having all of the following:1.Capable of measuring ions of 320 atomic mass units or greater and having a resolution of better than 1 part in 320;2.Ion sources constructed of or protected by nickel, nickel-copper alloys with a nickel content of 60 % or more by weight, or nickel-chrome alloys;3.Electron bombardment ionization sources;4.Having a collector system suitable for isotopic analysis.
0B001.d	7.Process systems for separating UF6 from carrier gas (hydrogen or helium) to 1 ppm UF6 content or less, including:a.Cryogenic heat exchangers and cryoseparators capable of temperatures of 153K (–120 °C) or less;b.Cryogenic refrigeration units capable of temperatures of 153 K (–120 °C) or less;c.Separation nozzle or vortex tube units for the separation of UF6 from carrier gas;d.UF6 cold traps capable of freezing out UF6;	TLB5.5.12	UF6/carrier gas separation systemsEspecially designed or prepared process systems for separating UF6 from carrier gas (hydrogen or helium).EXPLANATORY NOTE These systems are designed to reduce the UF6 content in the carrier gas to 1 ppm or less and may incorporate equipment such as:(a)Cryogenic heat exchangers and cryoseparators capable of temperatures of 153 K (–120 °C) or less, or(b)Cryogenic refrigeration units capable of temperatures of 153 K (–120 °C) or less, or(c)Separation nozzle or vortex tube units for the separation of UF6 from carrier gas, or(d)UF6 cold traps capable of freezing out UF6.
0B001.e	Equipment and components, specially designed or prepared for chemical exchange separation process, as follows:1.Fast-exchange liquid-liquid pulse columns with stage residence time of 30 seconds or less and resistant to concentrated hydrochloric acid (e.g. made of or protected by suitable plastic materials such as fluorinated hydrocarbon polymers or glass)	TLB5.6.1	Liquid-liquid exchange columns (Chemical exchange)Countercurrent liquid-liquid exchange columns having mechanical power input, especially designed or prepared for uranium enrichment using the chemical exchange process. For corrosion resistance to concentrated hydrochloric acid solutions, these columns and their internals are normally made of or protected by suitable plastic materials (such as fluorinated hydrocarbon polymers) or glass. The stage residence time of the columns is normally designed to be 30 seconds or less.
0B001.e	2.Fast-exchange liquid-liquid centrifugal contactors with stage residence time of 30 seconds or less and resistant to concentrated hydrochloric acid (e.g. made of or protected by suitable plastic materials such as fluorinated hydrocarbon polymers or glass);	TLB5.6.2	Liquid-liquid centrifugal contactors (Chemical exchange)Liquid-liquid centrifugal contactors especially designed or prepared for uranium enrichment using the chemical exchange process. Such contactors use rotation to achieve dispersion of the organic and aqueous streams and then centrifugal force to separate the phases. For corrosion resistance to concentrated hydrochloric acid solutions, the contactors are normally made of or protected by suitable plastic materials (such as fluorinated hydrocarbon polymers) or glass. The stage residence time of the centrifugal contactors is normally designed to be 30 seconds or less.
0B001.e	3.Electrochemical reduction cells resistant to concentrated hydrochloric acid solutions, for reduction of uranium from one valence state to another;	TLB5.6.3a	Uranium reduction systems and equipment (Chemical exchange)(a)Especially designed or prepared electrochemical reduction cells to reduce uranium from one valence state to another for uranium enrichment using the chemical exchange process. The cell materials in contact with process solutions must be corrosion resistant to concentrated hydrochloric acid solutions.EXPLANATORY NOTE The cell cathodic compartment must be designed to prevent re-oxidation of uranium to its higher valence state. To keep the uranium in the cathodic compartment, the cell may have an impervious diaphragm membrane constructed of special cation exchange material. The cathode consists of a suitable solid conductor such as graphite.
0B001.e	4.Electrochemical reduction cells feed equipment to take U+4 from the organic stream and, for those parts in contact with the process stream, made of or protected by suitable materials (e.g. glass, fluorocarbon polymers, polyphenyl sulphate, polyether sulfone and resin-impregnated graphite);	TLB5.6.3b	(b)Especially designed or prepared systems at the product end of the cascade for taking the U+4 out of the organic stream, adjusting the acid concentration and feeding to the electrochemical reduction cells.EXPLANATORY NOTE These systems consist of solvent extraction equipment for stripping the U+4 from the organic stream into an aqueous solution, evaporation and/or other equipment to accomplish solution pH adjustment and control, and pumps or other transfer devices for feeding to the electrochemical reduction cells. A major design concern is to avoid contamination of the aqueous stream with certain metal ions. Consequently, for those parts in contact with the process stream, the system is constructed of equipment made of or protected by suitable materials (such as glass, fluorocarbon polymers, polyphenyl sulfate, polyether sulfone, and resinimpregnated graphite).
0B001.e	5.Feed preparation systems for producing high purity uranium chloride solution consisting of dissolution, solvent extraction and/or ion exchange equipment for purification and electrolytic cells for reducing the uranium U+6 or U+4 to U+3;	TLB5.6.4	Feed preparation systems (Chemical exchange)Especially designed or prepared systems for producing high-purity uranium chloride feed solutions for chemical exchange uranium isotope separation plants.EXPLANATORY NOTE These systems consist of dissolution, solvent extraction and/or ion exchange equipment for purification and electrolytic cells for reducing the uranium U+6 or U+4 to U+3. These systems produce uranium chloride solutions having only a few parts per million of metallic impurities such as chromium, iron, vanadium, molybdenum and other bivalent or higher multi-valent cations. Materials of construction for portions of the system processing high-purity U+3 include glass, fluorinated hydrocarbon polymers, polyphenyl sulfate or polyether sulfone plastic-lined and resin-impregnated graphite. NSG Part 1 June 2013 - 39 - 5.6.5. Uranium
0B001.e	6.Uranium oxidation systems for oxidation of U+3 to U+4;	TLB5.6.5	Uranium oxidation systems (Chemical exchange)Especially designed or prepared systems for oxidation of U+3 to U+4 for return to the uranium isotope separation cascade in the chemical exchange enrichment process.EXPLANATORY NOTE These systems may incorporate equipment such as: (a) Equipment for contacting chlorine and oxygen with the aqueous effluent from the isotope separation equipment and extracting the resultant U+4 into the stripped organic stream returning from the product end of the cascade, (b) Equipment that separates water from hydrochloric acid so that the water and the concentrated hydrochloric acid may be reintroduced to the process at the proper locations.
0B001.f	Equipment and components, specially designed or prepared for ion-exchange separation process, as follows:1.Fast reacting ion-exchange resins, pellicular or porous macro-reticulated resins in which the active chemical exchange groups are limited to a coating on the surface of an inactive porous support structure, and other composite structures in any suitable form, including particles or fibres, with diameters of 0,2 mm or less, resistant to concentrated hydrochloric acid and designed to have an exchange rate half-time of less than 10 seconds and capable of operating at temperatures in the range of 373 K (100 °C) to 473 K (200 °C);	TLB5.6.6	Fast-reacting ion exchange resins/adsorbents (Ion exchange)Fast-reacting ion-exchange resins or adsorbents especially designed or prepared for uranium enrichment using the ion exchange process, including porous macroreticular resins, and/or pellicular structures in which the active chemical exchange groups are limited to a coating on the surface of an inactive porous support structure, and other composite structures in any suitable form including particles or fibres. These ion exchange resins/adsorbents have diameters of 0,2 mm or less and must be chemically resistant to concentrated hydrochloric acid solutions as well as physically strong enough so as not to degrade in the exchange columns. The resins/adsorbents are especially designed to achieve very fast uranium isotope exchange kinetics (exchange rate half-time of less than 10 seconds) and are capable of operating at a temperature in the range of 373 K (100 °C) to 473 K (200 °C).
0B001.f	2.Ion exchange columns (cylindrical) with a diameter greater than 1000 mm, made of or protected by materials resistant to concentrated hydrochloric acid (e.g. titanium or fluorocarbon plastics) and capable of operating at temperatures in the range of 373 K (100 °C) to 473 K (200 °C) and pressures above 0,7 MPa;	TLB5.6.7	Ion exchange columns (Ion exchange)Cylindrical columns greater than 1000 mm in diameter for containing and supporting packed beds of ion exchange resin/adsorbent, especially designed or prepared for uranium enrichment using the ion exchange process. These columns are made of or protected by materials (such as titanium or fluorocarbon plastics) resistant to corrosion by concentrated hydrochloric acid solutions and are capable of operating at a temperature in the range of 373 K (100 °C) to 473 K (200 °C) and pressures above 0,7 MPa.
0B001.f	3.Ion exchange reflux systems (chemical or electrochemical oxidation or reduction systems) for regeneration of the chemical reducing or oxidizing agents used in ion exchange enrichment cascades;	TLB5.6.8	Ion exchange reflux systems (Ion exchange)(a) Especially designed or prepared chemical or electrochemical reduction systems for regeneration of the chemical reducing agent(s) used in ion exchange uranium enrichment cascades. (b) Especially designed or prepared chemical or electrochemical oxidation systems for regeneration of the chemical oxidizing agent(s) used in ion exchange uranium enrichment cascades.
0B001.g	Equipment and components, specially designed or prepared for laser-based separation processes using atomic vapour laser isotope separation, as follows:1.Uranium metal vaporization systems designed to achieve a delivered power of 1 kW or more on the target for use in laser enrichment;	TLB5.7.1	Uranium vaporization systems (atomic vapour based methods)Especially designed or prepared uranium metal vaporization systems for use in laser enrichment.EXPLANATORY NOTE These systems may contain electron beam guns and are designed to achieve a delivered power (1 kW or greater) on the target sufficient to generate uranium metal vapour at a rate required for the laser enrichment function.
0B001.g	2.Liquid or vapour uranium metal handling systems specially designed or prepared for handling molten uranium, molten uranium alloys or uranium metal vapour for use in laser enrichment, and specially designed components therefor;N.B.:SEE ALSO 2A225.	TLB5.7.2	Liquid or vapour uranium metal handling systems and components (atomic vapour based methods)Especially designed or prepared systems for handling molten uranium, molten uranium alloys or uranium metal vapour for use in laser enrichment or especially designed or prepared components therefore.EXPLANATORY NOTE The liquid uranium metal handling systems may consist of crucibles and cooling equipment for the crucibles. The crucibles and other parts of this system that come into contact with molten uranium, molten uranium alloys or uranium metal vapour are made of or protected by materials of suitable corrosion and heat resistance. Suitable materials may include tantalum, yttria-coated graphite, graphite coated with other rare earth oxides (see INFCIRC/254/Part 2 — (as amended)) or mixtures thereof.
0B001.g	3.Product and tails collector assemblies for uranium metal in liquid or solid form, made of or protected by materials resistant to the heat and corrosion of uranium metal vapour or liquid, such as yttria-coated graphite or tantalum;	TLB5.7.3	Uranium metal "product" and "tails" collector assemblies (atomic vapour based methods)Especially designed or prepared "product" and "tails" collector assemblies for uranium metal in liquid or solid form.EXPLANATORY NOTE Components for these assemblies are made of or protected by materials resistant to the heat and corrosion of uranium metal vapour or liquid (such as yttria-coated graphite or tantalum) and may include pipes, valves, fittings, "gutters", feed-throughs, heat exchangers and collector plates for magnetic, electrostatic or other separation methods.
0B001.g	4.Separator module housings (cylindrical or rectangular vessels) for containing the uranium metal vapour source, the electron beam gun and the product and tails collectors;	TLB5.7.4	Separator module housings (atomic vapour based methods)Especially designed or prepared cylindrical or rectangular vessels for containing the uranium metal vapour source, the electron beam gun, and the "product" and "tails" collectors.EXPLANATORY NOTE These housings have multiplicity of ports for electrical and water feed-throughs, laser beam windows, vacuum pump connections and instrumentation diagnostics and monitoring. They have provisions for opening and closure to allow refurbishment of internal components.
0B001.g	5."Lasers" or "laser" systems specially designed or prepared for the separation of uranium isotopes with a spectrum frequency stabilisation for operation over extended periods of time;N.B.:SEE ALSO 6A005 AND 6A205.	TLB5.7.13	Laser systemsLasers or laser systems especially designed or prepared for the separation of uranium isotopes.EXPLANATORY NOTE The lasers and laser components of importance in laser-based enrichment processes include those identified in INFCIRC/254/Part 2 — (as amended). The laser system typically contains both optical and electronic components for the management of the laser beam (or beams) and the transmission to the isotope separation chamber. The laser system for atomic vapour based methods usually consists of tunable dye lasers pumped by another type of laser (e.g., copper vapour lasers or certain solid-state lasers). The laser system for molecular based methods may consist of CO2 lasers or excimer lasers and a multi-pass optical cell. Lasers or laser systems for both methods require spectrum frequency stabilization for operation over extended periods of time.
0B001.h	Equipment and components, specially designed or prepared for laser-based separation processes using molecular laser isotope separation, as follows:1.Supersonic expansion nozzles for cooling mixtures of UF6 and carrier gas to 150 K (–123 °C) or less and made from "materials resistant to corrosion by UF6";	TLB5.7.5	Supersonic expansion nozzles (molecular based methods)Especially designed or prepared supersonic expansion nozzles for cooling mixtures of UF6 and carrier gas to 150 K (–123 °C) or less and which are corrosion resistant to UF6.
0B001.h	2.Product or tails collector components or devices specially designed or prepared for collecting uranium material or uranium tails material following illumination with laser light, made of "materials resistant to corrosion by UF6";	TLB5.7.6	"Product" or "tails" collectors (molecular based methods)Especially designed or prepared components or devices for collecting uranium product material or uranium tails material following illumination with laser light.EXPLANATORY NOTE In one example of molecular laser isotope separation, the product collectors serve to collect enriched uranium pentafluoride (UF5) solid material. The product collectors may consist of filter, impact, or cyclone-type collectors, or combinations thereof, and must be corrosion resistant to the UF5/ UF6 environment.
0B001.h	3.Compressors made of or protected by "materials resistant to corrosion by UF6", and rotary shaft seals therefor;	TLB5.7.7	UF6/carrier gas compressors (molecular based methods)Especially designed or prepared compressors for UF6/carrier gas mixtures, designed for long term operation in a UF6 environment. The components of these compressors that come into contact with process gas are made of or protected by materials resistant to corrosion by UF6.
		TLB5.7.8	Rotary shaft seals (molecular based methods)Especially designed or prepared rotary shaft seals, with seal feed and seal exhaust connections, for sealing the shaft connecting the compressor rotor with the driver motor so as to ensure a reliable seal against out-leakage of process gas or in-leakage of air or seal gas into the inner chamber of the compressor which is filled with a UF6/carrier gas mixture.
0B001.h	4.Equipment for fluorinating UF5 (solid) to UF6 (gas);	TLB5.7.9	Fluorination systems (molecular based methods)Especially designed or prepared systems for fluorinating UF5 (solid) to UF6 (gas).EXPLANATORY NOTE These systems are designed to fluorinate the collected UF5 powder to UF6 for subsequent collection in product containers or for transfer as feed for additional enrichment. In one approach, the fluorination reaction may be accomplished within the isotope separation system to react and recover directly off the "product" collectors. In another approach, the UF5 powder may be removed/transferred from the "product" collectors into a suitable reaction vessel (e.g., fluidized-bed reactor, screw reactor or flame tower) for fluorination. In both approaches, equipment for storage and transfer of fluorine (or other suitable fluorinating agents) and for collection and transfer of UF6 are used.
0B001.h	5.Process systems for separating UF6 from carrier gas (e.g. nitrogen, argon or other gas) including:a.Cryogenic heat exchangers and cryoseparators capable of temperatures of 153 K (–120 °C) or less;b.Cryogenic refrigeration units capable of temperatures of 153 K (–120 °C) or less;c.UF6 cold traps capable of freezing out UF6;	TLB5.7.12	UF6/carrier gas separation systems (molecular based methods)Especially designed or prepared process systems for separating UF6 from carrier gas. EXPLANATORY NOTE These systems may incorporate equipment such as: (a) Cryogenic heat exchangers or cryoseparators capable of temperatures of 153 K (– 120 °C) or less, or (b) Cryogenic refrigeration units capable of temperatures of 153 K (–120 °C) or less, or (c) UF6 cold traps capable of freezing out UF6. The carrier gas may be nitrogen, argon, or other gas.
0B001.h	6."Lasers" or "laser" systems specially designed or prepared for the separation of uranium isotopes with a spectrum frequency stabilisation for operation over extended periods of time;N.B.:SEE ALSO 6A005 AND 6A205.	TLB5.7.13	Laser systemsLasers or laser systems especially designed or prepared for the separation of uranium isotopes.EXPLANATORY NOTE The lasers and laser components of importance in laser-based enrichment processes include those identified in INFCIRC/254/Part 2 — (as amended). The laser system typically contains both optical and electronic components for the management of the laser beam (or beams) and the transmission to the isotope separation chamber. The laser system for atomic vapour based methods usually consists of tunable dye lasers pumped by another type of laser (e.g., copper vapour lasers or certain solid-state lasers). The laser system for molecular based methods may consist of CO2 lasers or excimer lasers and a multi-pass optical cell. Lasers or laser systems for both methods require spectrum frequency stabilization for operation over extended periods of time.
0B001.i	Equipment and components, specially designed or prepared for plasma separation process, as follows:1.Microwave power sources and antennae for producing or accelerating ions, with an output frequency greater than 30 GHz and mean power output greater than 50 kW;	TLB5.8.1	Microwave power sources and antennaeEspecially designed or prepared microwave power sources and antennae for producing or accelerating ions and having the following characteristics: greater than 30 GHz frequency and greater than 50 kW mean power output for ion production.
0B001.i	2.Radio frequency ion excitation coils for frequencies of more than 100 kHz and capable of handling more than 40 kW mean power;	TLB5.8.2	Ion excitation coilsEspecially designed or prepared radio frequency ion excitation coils for frequencies of more than 100 kHz and capable of handling more than 40 kW mean power.
0B001.i	3.Uranium plasma generation systems;	TLB5.8.3	Uranium plasma generation systemsEspecially designed or prepared systems for the generation of uranium plasma for use in plasma separation plants.
0B001.i	4.Not used;	TLB5.8.4	No longer used — since 14 June 2013
0B001.i	5.Product and tails collector assemblies for uranium metal in solid form, made of or protected by materials resistant to the heat and corrosion of uranium vapour such as yttria-coated graphite or tantalum;	TLB5.8.5	Uranium metal "product" and "tails" collector assembliesEspecially designed or prepared "product" and "tails" collector assemblies for uranium metal in solid form. These collector assemblies are made of or protected by materials resistant to the heat and corrosion of uranium metal vapor, such as yttria-coated graphite or tantalum.
0B001.i	6.Separator module housings (cylindrical) for containing the uranium plasma source, radio-frequency drive coil and the product and tails collectors and made of a suitable non-magnetic material (e.g. stainless steel);	TLB.5.8.6	Separator module housings Cylindrical vessels especially designed or prepared for use in plasma separation enrichment plants for containing the uranium plasma source, radio-frequency drive coil and the "product" and "tails" collectors. EXPLANATORY NOTE These housings have a multiplicity of ports for electrical feed-throughs, diffusion pump connections and instrumentation diagnostics and monitoring. They have provisions for opening and closure to allow for refurbishment of internal components and are constructed of a suitable non-magnetic material such as stainless steel.
0B001.j	Equipment and components, specially designed or prepared for electromagnetic separation process, as follows:1.Ion sources, single or multiple, consisting of a vapour source, ioniser, and beam accelerator made of suitable non-magnetic materials (e.g. graphite, stainless steel, or copper) and capable of providing a total ion beam current of 50 mA or greater;	TLB5.9.1a	Electromagnetic isotope separatorsElectromagnetic isotope separators especially designed or prepared for the separation of uranium isotopes, and equipment and components therefor, including:(a)Ion sources Especially designed or prepared single or multiple uranium ion sources consisting of a vapour source, ionizer, and beam accelerator, constructed of suitable materials such as graphite, stainless steel, or copper, and capable of providing a total ion beam current of 50 mA or greater.
0B001.j	2.Ion collector plates for collection of enriched or depleted uranium ion beams, consisting of two or more slits and pockets and made of suitable non-magnetic materials (e.g. graphite or stainless steel);	TLB5.9.1b	Ion collectorsCollector plates consisting of two or more slits and pockets especially designed or prepared for collection of enriched and depleted uranium ion beams and constructed of suitable materials such as graphite or stainless steel.
0B001.j	3.Vacuum housings for uranium electromagnetic separators made of non-magnetic materials (e.g. stainless steel) and designed to operate at pressures of 0,1 Pa or lower;	TLB5.9.1c	Vacuum housingsEspecially designed or prepared vacuum housings for uranium electromagnetic separators, constructed of suitable non-magnetic materials such as stainless steel and designed for operation at pressures of 0,1 Pa or lower.EXPLANATORY NOTE The housings are specially designed to contain the ion sources, collector plates and water-cooled liners and have provision for diffusion pump connections and opening and closure for removal and reinstallation of these components.
0B001.j	4.Magnet pole pieces with a diameter greater than 2 m;	TLB5.9.1d	Magnet pole piecesEspecially designed or prepared magnet pole pieces having a diameter greater than 2 m used to maintain a constant magnetic field within an electromagnetic isotope separator and to transfer the magnetic field between adjoining separators.
0B001.j	5.High voltage power supplies for ion sources, having all of the following characteristics:a.Capable of continuous operation;b.Output voltage of 20000 V or greater;c.Output current of 1 A or greater; andd.Voltage regulation of better than 0,01 % over a period of 8 hours;N.B.:SEE ALSO 3A227.	TLB5.9.2	High voltage power suppliesEspecially designed or prepared high-voltage power supplies for ion sources, having all of the following characteristics: capable of continuous operation, output voltage of 20000 V or greater, output current of 1 A or greater, and voltage regulation of better than 0,01 % over a time period of 8 hours.
0B001.j	6.Magnet power supplies (high power, direct current) having all of the following characteristics:a.Capable of continuous operation with a current output of 500 A or greater at a voltage of 100 V or greater; andb.Current or voltage regulation better than 0,01 % over a period of 8 hours.N.B.:SEE ALSO 3A226.	TLB5.9.3	Magnet power suppliesEspecially designed or prepared high-power, direct current magnet power supplies having all of the following characteristics: capable of continuously producing a current output of 500 A or greater at a voltage of 100 V or greater and with a current or voltage regulation better than 0,01 % over a period of 8 hours.
0B002	Specially designed or prepared auxiliary systems, equipment and components, as follows, for isotope separation plant specified in 0B001, made of or protected by "materials resistant to corrosion by UF6":
0B002.a	Feed autoclaves, ovens or systems used for passing UF6 to the enrichment process;	TLB5.2.1	Feed systems/product and tails withdrawal systemsEspecially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
		TLB5.4.1	Feed systems/product and tails withdrawal systemsEspecially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
		TLB5.5.7	Feed systems/product and tails withdrawal systemsEspecially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers
		TLB5.7.11	Feed systems/product and tails withdrawal systems (molecular based methods)Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
0B002.b	Desublimers or cold traps, used to remove UF6 from the enrichment process for subsequent transfer upon heating;	TLB5.2.1	Feed systems/product and tails withdrawal systemsEspecially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
		TLB5.4.1	Feed systems/product and tails withdrawal systemsEspecially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
		TLB5.5.7	Feed systems/product and tails withdrawal systemsEspecially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
		TLB5.7.11	Feed systems/product and tails withdrawal systems (molecular based methods)Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
0B002.c	Product and tails stations for transferring UF6 into containers;	TLB5.2.1	Feed systems/product and tails withdrawal systemsEspecially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
		TLB5.4.1	Feed systems/product and tails withdrawal systemsEspecially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
		TLB5.5.7	Feed systems/product and tails withdrawal systemsEspecially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
		TLB5.7.11	Feed systems/product and tails withdrawal systems (molecular based methods)Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
0B002.d	Liquefaction or solidification stations used to remove UF6 from the enrichment process by compressing, cooling and converting UF6 to a liquid or solid form;	TLB5.2.1	Feed systems/product and tails withdrawal systemsEspecially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
		TLB5.4.1	Feed systems/product and tails withdrawal systemsEspecially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
		TLB5.5.7	Feed systems/product and tails withdrawal systemsEspecially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
		TLB5.7.11	Feed systems/product and tails withdrawal systems (molecular based methods)Especially designed or prepared process systems or equipment for enrichment plants made of or protected by materials resistant to corrosion by UF6, including: (a) Feed autoclaves, ovens, or systems used for passing UF6 to the enrichment process; (b) Desublimers (or cold traps) used to remove UF6 from the enrichment process for subsequent transfer upon heating; (c) Solidification or liquefaction stations used to remove UF6 from the enrichment process by compressing and converting UF6 to a liquid or solid form; (d) "Product" or "tails" stations used for transferring UF6 into containers.
0B002.e	Piping systems and header systems specially designed or prepared for handling UF6 within gaseous diffusion, centrifuge or aerodynamic cascades;	TLB5.2.2	Machine header piping systemsEspecially designed or prepared piping systems and header systems for handling UF6 within the centrifuge cascades. The piping network is normally of the "triple" header system with each centrifuge connected to each of the headers. There is thus a substantial amount of repetition in its form. It is wholly made of or protected by UF6-resistant materials (see EXPLANATORY NOTE to this section) and is fabricated to very high vacuum and cleanliness standards.
		TLB5.4.2	Header piping systemsEspecially designed or prepared piping systems and header systems for handling UF6 within the gaseous diffusion cascades.EXPLANATORY NOTE This piping network is normally of the "double" header system with each cell connected to each of the headers.
		TLB5.5.8	Header piping systemsEspecially designed or prepared header piping systems, made of or protected by materials resistant to corrosion by UF6, for handling UF6 within the aerodynamic cascades. This piping network is normally of the "double" header design with each stage or group of stages connected to each of the headers.
0B002.f	Vacuum systems and pumps as follows:1.Vacuum manifolds, vacuum headers or vacuum pumps having a suction capacity of 5 m3/minute or more;2.Vacuum pumps specially designed for use in UF6 bearing atmospheres made of, or protected by, "materials resistant to corrosion by UF6"; or3.Vacuum systems consisting of vacuum manifolds, vacuum headers and vacuum pumps, and designed for service in UF6-bearing atmospheres;	TLB5.4.3a	Vacuum systems(a)Especially designed or prepared vacuum manifolds, vacuum headers and vacuum pumps having a suction capacity of 5 m3 per minute or more.
		TLB5.4.3b	(b)Vacuum pumps especially designed for service in UF6-bearing atmospheres made of, or protected by, materials resistant to corrosion by UF6 (see EXPLANATORY NOTE to this section). These pumps may be either rotary or positive, may have displacement and fluorocarbon seals, and may have special working fluids present.
		TLB5.5.9b	Vacuum systems and pumpsVacuum pumps especially designed or prepared for service in UF6-bearing atmospheres and made of or protected by materials resistant to corrosion by UF6. These pumps may use fluorocarbon seals and special working fluids.
		TLB5.5.9a	Especially designed or prepared vacuum systems consisting of vacuum manifolds, vacuum headers and vacuum pumps, and designed for service in UF6-bearing atmospheres
0B002.g	UF6 mass spectrometers/ion sources capable of taking on-line samples from UF6 gas streams and having all of the following:1.Capable of measuring ions of 320 atomic mass units or greater and having a resolution of better than 1 part in 320;2.Ion sources constructed of or protected by nickel, nickel-copper alloys with a nickel content of 60 % or more by weight, or nickel-chrome alloys;3.Electron bombardment ionisation sources; and4.Having a collector system suitable for isotopic analysis.	TLB5.2.4	UF6 mass spectrometers/ion sourcesEspecially designed or prepared mass spectrometers capable of taking on-line samples from UF6 gas streams and having all of the following:1.Capable of measuring ions of 320 atomic mass units or greater and having a resolution of better than 1 part in 320;2.Ion sources constructed of or protected by nickel, nickel-copper alloys with a nickel content of 60 % or more by weight, or nickel-chrome alloys;3.Electron bombardment ionization sources;4.Having a collector system suitable for isotopic analysis.
		TLB5.4.5	UF6 mass spectrometers/ion sourcesEspecially designed or prepared mass spectrometers capable of taking on-line samples from UF6 gas streams and having all of the following:1.Capable of measuring ions of 320 atomic mass units or greater and having a resolution of better than 1 part in 320;2.Ion sources constructed of or protected by nickel, nickel-copper alloys with a nickel content of 60 % or more by weight, or nickel-chrome alloys;3.Electron bombardment ionization sources;4.Having a collector system suitable for isotopic analysis.
		TLB5.5.11	UF6 mass spectrometers/Ion sourcesEspecially designed or prepared mass spectrometers capable of taking on-line samples from UF6 gas streams and having all of the following:1.Capable of measuring ions of 320 atomic mass units or greater and having a resolution of better than 1 part in 320;2.Ion sources constructed of or protected by nickel, nickel-copper alloys with a nickel content of 60 % or more by weight, or nickel-chrome alloys;3.Electron bombardment ionization sources;4.Having a collector system suitable for isotopic analysis.
		TLB5.7.10	Special shut-off and control valvesEspecially designed or prepared bellows-sealed valves, manual or automated, shut-off or control, made of or protected by materials resistant to corrosion by UF6, with a diameter of 40 mm or greater, for installation in main and auxiliary systems of aerodynamic enrichment plants.
0B003	Plant for the conversion of uranium and equipment specially designed or prepared therefor, as follows:	TLB7.1	Especially designed or prepared systems for the conversion of uranium ore concentrates to UO3
0B003.a	Systems for the conversion of uranium ore concentrates to UO3;	TLB7.1.1	EXPLANATORY NOTE Conversion of uranium ore concentrates to UO3 can be performed by first dissolving the ore in nitric acid and extracting purified uranyl nitrate using a solvent such as tributyl phosphate. Next, the uranyl nitrate is converted to UO3 either by concentration and denitration or by neutralization with gaseous ammonia to produce ammonium diuranate with subsequent filtering, drying, and calcining
0B003.b	Systems for the conversion of UO3 to UF6;	TLB7.1.2	Especially designed or prepared systems for the conversion of UO3 to UF6 EXPLANATORY NOTEEXPLANATORY NOTE Conversion of UO3 to UO2 can be performed through reduction of UO3 with cracked ammonia gas or hydrogen.
0B003.c	Systems for the conversion of UO3 to UO2;	TLB7.1.3	Especially designed or prepared systems for the conversion of UO3 to UO2EXPLANATORY NOTE Conversion of UO3 to UO2 can be performed through reduction of UO3 with cracked ammonia gas or hydrogen.
0B003.d	Systems for the conversion of UO2 to UF4;	TLB7.1.4	Especially designed or prepared systems for the conversion of UO2 to UF4EXPLANATORY NOTE Conversion of UO2 to UF4 can be performed by reacting UO2 with hydrogen fluoride gas (HF) at 300-500 °C.
0B003.e	Systems for the conversion of UF4 to UF6;	TLB7.1.5	Especially designed or prepared systems for the conversion of UF4 to UF6EXPLANATORY NOTE Conversion of UF4 to UF6 is performed by exothermic reaction with fluorine in a tower reactor. UF6 is condensed from the hot effluent gases by passing the effluent stream through a cold trap cooled to –10 °C. The process requires a source of fluorine gas
0B003.f	Systems for the conversion of UF4 to uranium metal;	TLB7.1.6	Especially designed or prepared systems for the conversion of UF4 to U metalEXPLANATORY NOTE Conversion of UF4 to U metal is performed by reduction with magnesium (large batches) or calcium (small batches). The reaction is carried out at temperatures above the melting point of uranium (1130 °C).
0B003.g	Systems for the conversion of UF6 to UO2;	TLB7.1.7	Especially designed or prepared systems for the conversion of UF6 to UO2EXPLANATORY NOTE Conversion of UF6 to UO2 can be performed by one of three processes. In the first, UF6 is reduced and hydrolyzed to UO2 using hydrogen and steam. In the second, UF6 is hydrolyzed by solution in water, ammonia is added to precipitate ammonium diuranate, and the diuranate is reduced to UO2 with hydrogen at 820 °C. In the third process, gaseous UF6, CO2, and NH3 are combined in water, precipitating ammonium uranyl carbonate. The ammonium uranyl carbonate is combined with steam and hydrogen at 500-600 °C to yield UO2. UF6 to UO2 conversion is often performed as the first stage of a fuel fabrication plant.
0B003.h	Systems for the conversion of UF6 to UF4;	TLB7.1.8	Especially designed or prepared systems for the conversion of UF6 to UF4EXPLANATORY NOTE Conversion of UF6 to UF4 is performed by reduction with hydrogen.
0B003.i	Systems for the conversion of UO2 to UCl4.	TLB7.1.9	Especially designed or prepared systems for the conversion of UO2 to UCl4EXPLANATORY NOTE Conversion of UO2 to UCl4 can be performed by one of two processes. In the first, UO2 is reacted with carbon tetrachloride (CCl4) at approximately 400 °C. In the second, UO2 is reacted at approximately 700 °C in the presence of carbon black (CAS 1333-86-4), carbon monoxide, and chlorine to yield UCl4.
0B004	Plant for the production or concentration of heavy water, deuterium and deuterium compounds and specially designed or prepared equipment and components therefor, as follows:	TLB6	Plants for the production or concentration of heavy water, deuterium and deuterium compounds and equipment especially designed or prepared therefor:
0B004.a	Plant for the production of heavy water, deuterium or deuterium compounds, as follows:1.Water-hydrogen sulphide exchange plants;2.Ammonia-hydrogen exchange plants;
0B004.b	Equipment and components, as follows:
	1.Water-hydrogen sulphide exchange towers with diameters of 1,5 m or more, capable of operating at pressures greater than or equal to 2 MPa;	TLB6.1	Water — Hydrogen Sulphide Exchange Towers Exchange towers with diameters of 1,5 m or greater and capable of operating at pressures greater than or equal to 2 MPa (300 psi), especially designed or prepared for heavy water production utilizing the water-hydrogen sulphide exchange process.
	2.Single stage, low head (i.e. 0,2 MPa) centrifugal blowers or compressors for hydrogen sulphide gas circulation (i.e. gas containing more than 70 % H2S) with a throughput capacity greater than or equal to 56 m3/second when operating at pressures greater than or equal to 1,8 MPa suction and having seals designed for wet H2S service;	TLB6.2	Blowers and CompressorsSingle stage, low head (i.e., 0,2 MPa or 30 psi) centrifugal blowers or compressors for hydrogen-sulphide gas circulation (i.e., gas containing more than 70 % H2S) especially designed or prepared for heavy water production utilizing the water-hydrogen sulphide exchange process. These blowers or compressors have a throughput capacity greater than or equal to 56 m3/second (120000 SCFM) while operating at pressures greater than or equal to 1,8 MPa (260 psi) suction and have seals designed for wet H2S service.
	3.Ammonia-hydrogen exchange towers greater than or equal to 35 m in height with diameters of 1,5 m to 2,5 m capable of operating at pressures greater than 15 MPa;	TLB6.3	Ammonia-Hydrogen Exchange TowersAmmonia-hydrogen exchange towers greater than or equal to 35 m (114,3 ft) in height with diameters of 1,5 m (4,9 ft) to 2,5 m (8,2 ft) capable of operating at pressures greater than 15 MPa (2225 psi) especially designed or prepared for heavy water production utilizing the ammonia-hydrogen exchange process. These towers also have at least one flanged, axial opening of the same diameter as the cylindrical part through which the tower internals can be inserted or withdrawn.
	4.Tower internals, including stage contactors, and stage pumps, including those which are submersible, for heavy water production utilizing the ammonia-hydrogen exchange process;	TLB6.4	Tower Internals and Stage PumpsTower internals and stage pumps especially designed or prepared for towers for heavy water production utilizing the ammonia-hydrogen exchange process. Tower internals include especially designed stage contactors which promote intimate gas/liquid contact. Stage pumps include especially designed submersible pumps for circulation of liquid ammonia within a contacting stage internal to the stage towers.
	5.Ammonia crackers with operating pressures greater than or equal to 3 MPa for heavy water production utilizing the ammonia-hydrogen exchange process;	TLB6.5	Ammonia CrackersAmmonia crackers with operating pressures greater than or equal to 3 MPa (450 psi) especially designed or prepared for heavy water production utilizing the ammoniahydrogen exchange process.
	6.Infrared absorption analysers capable of on-line hydrogen/deuterium ratio analysis where deuterium concentrations are equal to or greater than 90 %;	TLB6.6	Infrared Absorption AnalyzersInfrared absorption analyzers capable of "on-line" hydrogen/deuterium ratio analysis where deuterium concentrations are equal to or greater than 90 %.
	7.Catalytic burners for the conversion of enriched deuterium gas into heavy water utilizing the ammonia-hydrogen exchange process;	TLB6.7	Catalytic BurnersCatalytic burners for the conversion of enriched deuterium gas into heavy water especially designed or prepared for heavy water production utilizing the ammoniahydrogen exchange process.
	8.Complete heavy water upgrade systems, or columns therefor, for the upgrade of heavy water to reactor-grade deuterium concentration;	TLB6.8	Complete heavy water upgrade systems or columns thereforComplete heavy water upgrade systems, or columns therefor, especially designed or prepared for the upgrade of heavy water to reactor-grade deuterium concentration.EXPLANATORY NOTE These systems, which usually employ water distillation to separate heavy water from light water, are especially designed or prepared to produce reactor-grade heavy water (i.e., typically 99,75 % deuterium oxide) from heavy water feedstock of lesser concentration.
	9.Ammonia synthesis converters or synthesis units specially designed or prepared for heavy water production utilizing the ammonia-hydrogen exchange process	TLB6.9	Ammonia synthesis converters or synthesis unitsAmmonia synthesis converters or synthesis units especially designed or prepared for heavy water production utilizing the ammonia-hydrogen exchange process.EXPLANATORY NOTE These converters or units take synthesis gas (nitrogen and hydrogen) from an ammonia/hydrogen high-pressure exchange column (or columns), and the synthesized ammonia is returned to the exchange column (or columns).
0B005	Plant specially designed for the fabrication of "nuclear reactor" fuel elements and specially designed or prepared equipment therefor.Technical Note:Specially designed or prepared equipment for the fabrication of "nuclear reactor" fuel elements includes equipment which:1.Normally comes into direct contact with or directly processes or controls the production flow of nuclear materials;2.Seals the nuclear materials within the cladding;3.Checks the integrity of the cladding or the seal;4.Checks the finish treatment of the sealed fuel; or5.Is used for assembling reactor elements.		Plants for the fabrication of nuclear reactor fuel elements, and equipment especially designed or prepared thereforINTRODUCTORY NOTE Nuclear fuel elements are manufactured from one or more of the source or special fissionable materials mentioned in MATERIAL AND EQUIPMENT of this annex. For oxide fuels, the most common type of fuel, equipment for pressing pellets, sintering, grinding and grading will be present. Mixed oxide fuels are handled in glove boxes (or equivalent containment) until they are sealed in the cladding. In all cases, the fuel is hermetically sealed inside a suitable cladding which is designed to be the primary envelope encasing the fuel so as to provide suitable performance and safety during reactor operation. Also, in all cases, precise control of processes, procedures and equipment to extremely high standards is necessary in order to ensure predictable and safe fuel performance.EXPLANATORY NOTE Items of equipment that are considered to fall within the meaning of the phrase "and equipment especially designed or prepared" for the fabrication of fuel elements include equipment which: (a) normally comes in direct contact with, or directly processes, or controls, the production flow of nuclear material; (b) seals the nuclear material within the cladding; (c) checks the integrity of the cladding or the seal; (d) checks the finish treatment of the sealed fuel; or (e) is used for assembling reactor fuel elements. Such equipment or systems of equipment may include, for example: 1) fully automatic pellet inspection stations especially designed or prepared for checking final dimensions and surface defects of the fuel pellets; 2) automatic welding machines especially designed or prepared for welding end caps onto the fuel pins (or rods); 3) automatic test and inspection stations especially designed or prepared for checking the integrity of completed fuel pins (or rods); 4) systems especially designed or prepared to manufacture nuclear fuel cladding. Item 3 typically includes equipment for: a) x-ray examination of pin (or rod) end cap welds, b) helium leak detection from pressurized pins (or rods), and c) gamma-ray scanning of the pins (or rods) to check for correct loading of the fuel pellets inside.
0B006	Plant for the reprocessing of irradiated "nuclear reactor" fuel elements, and specially designed or prepared equipment and components therefor.Note:0B006 includes:a.Plant for the reprocessing of irradiated "nuclear reactor" fuel elements including equipment and components which normally come into direct contact with and directly control the irradiated fuel and the major nuclear material and fission product processing streams;	TLB3	Plants for the reprocessing of irradiated fuel elements, and equipment especially designed or prepared thereforINTRODUCTORY NOTEReprocessing irradiated nuclear fuel separates plutonium and uranium from intensely radioactive fission products and other transuranic elements. Different technical processes can accomplish this separation. However, over the years Purex has become the most commonly used and accepted process. Purex involves the dissolution of irradiated nuclear fuel in nitric acid, followed by separation of the uranium, plutonium, and fission products by solvent extraction using a mixture of tributyl phosphate in an organic diluent. Purex facilities have process functions similar to each other, including: irradiated fuel element chopping, fuel dissolution, solvent extraction, and process liquor storage. There may also be equipment for thermal denitration of uranium nitrate, conversion of plutonium nitrate to oxide or metal, and treatment of fission product waste liquor to a form suitable for long term storage or disposal. However, the specific type and configuration of the equipment performing these functions may differ between Purex facilities for several reasons, including the type and quantity of irradiated nuclear fuel to be reprocessed and the intended disposition of the recovered materials, and the safety and maintenance philosophy incorporated into the design of the facility. A "plant for the reprocessing of irradiated fuel elements", includes the equipment and components which normally come in direct contact with and directly control the irradiated fuel and the major nuclear material and fission product processing streams. These processes, including the complete systems for plutonium conversion and plutonium metal production, may be identified by the measures taken to avoid criticality (e.g. by geometry), radiation exposure (e.g. by shielding), and toxicity hazards (e.g. by containment).
	b.Fuel element chopping or shredding machines, i.e. remotely operated equipment to cut, chop or shear irradiated "nuclear reactor" fuel assemblies, bundles or rods;	TLB3.1	Irradiated fuel element chopping machinesRemotely operated equipment especially designed or prepared for use in a reprocessing plant as identified above and intended to cut, chop or shear irradiated nuclear fuel assemblies, bundles or rods.EXPLANATORY NOTE This equipment breaches the cladding of the fuel to expose the irradiated nuclear material to dissolution. Especially designed metal cutting shears are the most commonly employed, although advanced equipment, such as lasers, may be used.
	c.Dissolvers, critically safe tanks (e.g. small diameter, annular or slab tanks) specially designed or prepared for the dissolution of irradiated "nuclear reactor" fuel, which are capable of withstanding hot, highly corrosive liquids, and which can be remotely loaded and maintained;	TLB3.2	DissolversCritically safe tanks (e.g. small diameter, annular or slab tanks) especially designed or prepared for use in a reprocessing plant as identified above, intended for dissolution of irradiated nuclear fuel and which are capable of withstanding hot, highly corrosive liquid, and which can be remotely loaded and maintained.EXPLANATORY NOTE Dissolvers normally receive the chopped-up spent fuel. In these critically safe vessels, the irradiated nuclear material is dissolved in nitric acid and the remaining hulls removed from the process stream.
	d.Solvent extractors, such as packed or pulsed columns, mixer settlers or centrifugal contractors, resistant to the corrosive effects of nitric acid and specially designed or prepared for use in a plant for the reprocessing of irradiated "natural uranium", "depleted uranium" or "special fissile materials";	TLB3.3	Solvent extractors and solvent extraction equipmentEspecially designed or prepared solvent extractors such as packed or pulse columns, mixer settlers or centrifugal contactors for use in a plant for the reprocessing of irradiated fuel. Solvent extractors must be resistant to the corrosive effect of nitric acid. Solvent extractors are normally fabricated to extremely high standards (including special welding and inspection and quality assurance and quality control techniques) out of low carbon stainless steels, titanium, zirconium, or other high quality materials.EXPLANATORY NOTE Solvent extractors both receive the solution of irradiated fuel from the dissolvers and the organic solution which separates the uranium, plutonium, and fission products. Solvent extraction equipment is normally designed to meet strict operating parameters, such as long operating lifetimes with no maintenance requirements or adaptability to easy replacement, simplicity of operation and control, and flexibility for variations in process conditions.
	e.Holding or storage vessels specially designed to be critically safe and resistant to the corrosive effects of nitric acid;Technical Note:Holding or storage vessels may have the following features:1.Walls or internal structures with a boron equivalent (calculated for all constituent elements as defined in the note to 0C004) of at least two per cent;2.A maximum diameter of 175 mm for cylindrical vessels; or3.A maximum width of 75 mm for either a slab or annular vessel.	TLB3.4	Chemical holding or storage vesselsEspecially designed or prepared holding or storage vessels for use in a plant for the reprocessing of irradiated fuel. The holding or storage vessels must be resistant to the corrosive effect of nitric acid. The holding or storage vessels are normally fabricated of materials such as low carbon stainless steels, titanium or zirconium, or other high quality materials. Holding or storage vessels may be designed for remote operation and maintenance and may have the following features for control of nuclear criticality:(1)walls or internal structures with a boron equivalent of at least two per cent, or(2)a maximum diameter of 175 mm (7 in) for cylindrical vessels, or(3)a maximum width of 75 mm (3 in) for either a slab or annular vessel.EXPLANATORY NOTE Three main process liquor streams result from the solvent extraction step. Holding or storage vessels are used in the further processing of all three streams, as follows:(a)The pure uranium nitrate solution is concentrated by evaporation and passed to a denitration process where it is converted to uranium oxide. This oxide is re-used in the nuclear fuel cycle.(b)The intensely radioactive fission products solution is normally concentrated by evaporation and stored as a liquor concentrate. This concentrate may be subsequently evaporated and converted to a form suitable for storage or disposal.(c)The pure plutonium nitrate solution is concentrated and stored pending its transfer to further process steps. In particular, holding or storage vessels for plutonium solutions are designed to avoid criticality problems resulting from changes in concentration and form of this stream.
	f.Neutron measurement systems specially designed or prepared for integration and use with automated process control systems in a plant for the reprocessing of irradiated "natural uranium", "depleted uranium" or "special fissile materials".	TLB3.5	Neutron measurement systems for process controlNeutron measurement systems especially designed or prepared for integration and use with automated process control systems in a plant for the reprocessing of irradiated fuel elements.EXPLANATORY NOTE These systems involve the capability of active and passive neutron measurement and discrimination in order to determine the fissile material quantity and composition. The complete system is composed of a neutron generator, a neutron detector, amplifiers, and signal processing electronics. The scope of this entry does not include neutron detection and measurement instruments that are designed for nuclear material accountancy and safeguarding or any other application not related to integration and use with automated process control systems in a plant for the reprocessing of irradiated fuel elements.
0B007	Plant for the conversion of plutonium and equipment specially designed or prepared therefor, as follows:	TLB7.2.1	Especially designed or prepared systems for the conversion of plutonium nitrate to oxide
0B007.a	a.Systems for the conversion of plutonium nitrate to oxide;		EXPLANATORY NOTE The main functions involved in this process are: process feed storage and adjustment, precipitation and solid/liquor separation, calcination, product handling, ventilation, waste management, and process control. The process systems are particularly adapted so as to avoid criticality and radiation effects and to minimize toxicity hazards. In most reprocessing facilities, this process involves the conversion of plutonium nitrate to plutonium dioxide. Other processes can involve the precipitation of plutonium oxalate or plutonium peroxide.
0B007.b	b.Systems for plutonium metal production.	TLB7.2.2	Especially designed or prepared systems for plutonium metal productionEXPLANATORY NOTE This process usually involves the fluorination of plutonium dioxide, normally with highly corrosive hydrogen fluoride, to produce plutonium fluoride which is subsequently reduced using high purity calcium metal to produce metallic plutonium and a calcium fluoride slag. The main functions involved in this process are fluorination (e.g. involving equipment fabricated or lined with a precious metal), metal reduction (e.g. employing ceramic crucibles), slag recovery, product handling, ventilation, waste management and process control. The process systems are particularly adapted so as to avoid criticality and radiation effects and to minimize toxicity hazards. Other processes include the fluorination of plutonium oxalate or plutonium peroxide followed by a reduction to metal.
0C001	"Natural uranium" or "depleted uranium" or thorium in the form of metal, alloy, chemical compound or concentrate and any other material containing one or more of the foregoing;Note:0C001 does not control the following:a.Four grammes or less of "natural uranium" or "depleted uranium" when contained in a sensing component in instruments;b."Depleted uranium" specially fabricated for the following civil non-nuclear applications:1.Shielding;2.Packaging;3.Ballasts having a mass not greater than 100 kg;4.Counter-weights having a mass not greater than 100 kg;c.Alloys containing less than 5 % thorium;d.Ceramic products containing thorium, which have been manufactured for non-nuclear use.	TLA.1.1	1.1."Source material"The term "source material" means uranium containing the mixture of isotopes occurring in nature; uranium depleted in the isotope 235; thorium; any of the foregoing in the form of metal, alloy, chemical compound, or concentrate; any other material containing one or more of the foregoing in such concentration as the Board of Governors shall from time to time determine; and such other material as the Board of Governors shall from time to time determine.
0C002	"Special fissile materials"Note:0C002 does not control four "effective grammes" or less when contained in a sensing component in instruments.	TLA.1.2	1.2."Special fissionable material"i)The term "special fissionable material" means plutonium-239; uranium-233; "uranium enriched in the isotopes 235 or 233"; any material containing one or more of the foregoing; and such other fissionable material as the Board of Governors shall from time to time determine; but the term "special fissionable material" does not include source material.ii)The term "uranium enriched in the isotopes 235 or 233" means uranium containing the isotopes 235 or 233 or both in an amount such that the abundance ratio of the sum of these isotopes to the isotope 238 is greater than the ratio of the isotope 235 to the isotope 238 occurring in nature.However, for the purposes of the Guidelines, items specified in subparagraph (a) below, and exports of source or special fissionable material to a given recipient country, within a period of 12 months, below the limits specified in subparagraph (b) below, shall not be included:(a)Plutonium with an isotopic concentration of plutonium-238 exceeding 80 %.Special fissionable material when used in gram quantities or less as a sensing component in instruments; andSource material which the Government is satisfied is to be used only in non-nuclear activities, such as the production of alloys or ceramics;(b)Special fissionable material50 effective grams;Natural uranium500 kilograms;Depleted uranium1000 kilograms; andThorium1000 kilograms.
0C003	Deuterium, heavy water (deuterium oxide) and other compounds of deuterium, and mixtures and solutions containing deuterium, in which the isotopic ratio of deuterium to hydrogen exceeds 1:5000.	TLB2.1	2.1.Deuterium and heavy waterDeuterium, heavy water (deuterium oxide) and any other deuterium compound in which the ratio of deuterium to hydrogen atoms exceeds 1:5000 for use in a nuclear reactor as defined in paragraph 1.1. above in quantities exceeding 200 kg of deuterium atoms for any one recipient country in any period of 12 months.
0C004	Graphite having a purity level better than 5 parts per million "boron equivalent" and with a density greater than 1,50 g/cm3 for use in a "nuclear reactor", in quantities exceeding 1 kg.N.B.:SEE ALSO 1C107Note 1:For the purpose of export control, the competent authorities of the Member State in which the exporter is established will determine whether or not the exports of graphite meeting the above specifications are for "nuclear reactor" use.Note 2:In 0C004, "boron equivalent" (BE) is defined as the sum of BEz for impurities (excluding BEcarbon since carbon is not considered an impurity) including boron, where:BEZ (ppm) = CF × concentration of element Z in ppm;and σB and σZ are the thermal neutron capture cross sections (in barns) for naturally occurring boron and element Z respectively; and AB and AZ are the atomic masses of naturally occurring boron and element Z respectively.	TLB2.2	2.2.Nuclear grade graphiteGraphite having a purity level better than 5 parts per million boron equivalent and with a density greater than 1,50 g/cm3 for use in a nuclear reactor as defined in paragraph 1.1 above, in quantities exceeding 1 kilogram.EXPLANATORY NOTEFor the purpose of export control, the Government will determine whether or not the exports of graphite meeting the above specifications are for nuclear reactor use.Boron equivalent (BE) may be determined xperimentally or is calculated as the sum of BEz for impurities (excluding BEcarbon since carbon is not considered an impurity) including boron, where:BEZ (ppm) = CF × concentration of element Z (in ppm);CF is the conversion factor: (σZ × AB) divided by (σB × Az);σB and σZ are the thermal neutron capture cross sections (in barns) for naturally occurring boron and element Z respectively; and AB and Az are the atomic masses of naturally occurring boron and element Z respectively.
0C005	Specially prepared compounds or powders for the manufacture of gaseous diffusion barriers, resistant to corrosion by UF6 (e.g. nickel or alloy containing 60 weight per cent or more nickel, aluminium oxide and fully fluorinated hydrocarbon polymers), having a purity of 99,9 % by weight or more and a particle size less than 10 μm measured by American Society for Testing and Materials (ASTM) B330 standard and a high degree of particle size uniformity.	TLB5.3.1b	Gaseous diffusion barriers and barrier materials(b)especially prepared compounds or powders for the manufacture of such filters.Such compounds and powders include nickel or alloys containing 60 % or more nickel, aluminium oxide, or UF6-resistant fully fluorinated hydrocarbon polymers having a purity of 99,9 % by weight or more, a particle size less than 10 μm, and a high degree of particle size uniformity, which are especially prepared for the manufacture of gaseous diffusion barriers.
OD001	T*"Software" specially designed or modified for the "development", "production" or "use" of goods specified in this Category.II*IV*	TLB*	"software" means a collection of one or more "programs" or "microprograms" fixed in any tangible medium of expression. "technical assistance" may take forms such as: instruction, skills, training, working knowledge, consulting services.
0E001	T* "Technology" according to the Nuclear Technology Note for the "development", "production" or "use" of goods specified in this Category.II*IV	TLB*	"technology" means specific information required for the "development", "production", or "use" of any item contained in the List. This information may take the form of "technical data", or "technical assistance".

CATEGORY 1 — SPECIAL MATERIALS AND RELATED EQUIPMENT1ASystems, Equipment and Components

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
1A007	b.Electrically driven explosive detonators as follows:1.Exploding bridge (EB);2.Exploding bridge wire (EBW);3.Slapper;4.Exploding foil initiators (EFI).Technical Notes:1.The word initiator or igniter is sometimes used in place of the word detonator.2.For the purpose of 1A007.b. the detonators of concern all utilise a small electrical conductor (bridge, bridge wire, or foil) that explosively vaporises when a fast, high-current electrical pulse is passed through it. In non-slapper types, the exploding conductor starts a chemical detonation in a contacting high explosive material such as PETN (pentaerythritoltetranitrate). In3.slapper detonators, the explosive vaporization of the electrical conductor drives a flyer or slapper across a gap, and the impact of the slapper on an explosive starts a chemical detonation. The slapper in some designs is driven by magnetic force. The term exploding foil detonator may refer to either an EB or a slapper-type detonator.	6.A.1.	Detonators and multipoint initiation systems, as follows:a.Electrically driven explosive detonators, as follows:1.Exploding bridge (EB);2.Exploding bridge wire (EBW);3.Slapper;4.Exploding foil initiators (EFI);
1A007	Equipment and devices, specially designed to initiate charges and devices containing "energetic materials", by electrical means, as follows:N.B.:SEE ALSO MILITARY GOODS CONTROLS, 3A229 AND 3A232.a.Explosive detonator firing sets designed to drive explosive detonators specified in 1A007.b.;	6.A.2.	Firing sets and equivalent high-current pulse generators, as follows:a.Detonator firing sets (initiation systems, firesets), including electronically-charged, explosively-driven and optically-driven firing sets designed to drive multiple controlled detonators specified by Item 6.A.1. above;
1A202	Composite structures, other than those specified in 1A002, in the form of tubes and having both of the following characteristics:N.B.:SEE ALSO 9A010 AND 9A110.a.An inside diameter of between 75 mm and 400 mm; andb.Made with any of the "fibrous or filamentary materials" specified in 1C010.a. or b. or 1C210.a. or with carbon prepreg materials specified in 1C210.c.	2.A.3.	Composite structures in the form of tubes having both of the following characteristics:a.An inside diameter of between 75 and 400 mm; andb.Made with any of the "fibrous or filamentary materials" specified in Item 2.C.7.a. or carbon prepreg materials specified in Item 2.C.7.c.
1A225	Platinized catalysts specially designed or prepared for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water.	2.A.2.	Platinized catalysts specially designed or prepared for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water.
1A226	Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics:a.Made of phosphor bronze mesh chemically treated to improve wettability; andb.Designed to be used in vacuum distillation towers.	4.A.1.	Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics:a.Made of phosphor bronze mesh chemically treated to improve wettability; andb.Designed to be used in vacuum distillation towers.
1A227	High-density (lead glass or other) radiation shielding windows, having all of the following characteristics, and specially designed frames therefor:a.A "cold area" greater than 0,09 m2;b.A density greater than 3 g/cm3; andc.A thickness of 100 mm or greater.Technical Note:In 1A227 the term "cold area" means the viewing area of the window exposed to the lowest level of radiation in the design application.	1.A.1.	High-density (lead glass or other) radiation shielding windows, having all of the following characteristics, and specially designed frames therefor:a.A "cold area" greater than 0,09 m2;b.A density greater than 3 g/cm3; andc.A thickness of 100 mm or greater.Technical Note:In Item 1.A.1.a. the term "cold area" means the viewing area of the window exposed to the lowest level of radiation in the design application.

1BTest, Inspection and Production Equipment

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
1B201	Filament winding machines, other than those specified in 1B001 or 1B101, and related equipment, as follows:a.Filament winding machines having all of the following characteristics:1.Having motions for positioning, wrapping, and winding fibres coordinated and programmed in two or more axes;2.Specially designed to fabricate composite structures or laminates from "fibrous or filamentary materials"; and3.Capable of winding cylindrical tubes with an internal diameter between 75 and 650 mm and lengths of 300 mm or greater;b.Coordinating and programming controls for the filament winding machines specified in 1B201.a.;c.Precision mandrels for the filament winding machines specified in 1B201.a.	3.B.4.	Filament winding machines and related equipment, as follows:a.Filament winding machines having all of the following characteristics:1.Having motions for positioning, wrapping, and winding fibers coordinated and programmed in two or more axes;2.Specially designed to fabricate composite structures or laminates from "fibrous or filamentary materials"; and3.Capable of winding cylindrical tubes with an internal diameter between 75 and 650 mm and lengths of 300 mm or greater;b.Coordinating and programming controls for the filament winding machines specified in Item 3.B.4.a.;c.Precision mandrels for the filament winding machines specified in Item 3.B.4.a.
1B225	Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour.	3.B.1.	Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour.
1B226	Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater.Note:1B226 includes separators:a.Capable of enriching stable isotopes;b.With the ion sources and collectors both in the magnetic field and those configurations in which they are external to the field.	3.B.5.	Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater.Notes:1.Item 3.B.5. includes separators capable of enriching stable isotopes as well as those for uranium.N.B.:A separator capable of separating the isotopes of lead with a one-mass unit difference is inherently capable of enriching the isotopes of uranium with a three-unit mass difference.2.Item 3.B.5. includes separators with the ion sources and collectors both in the magnetic field and those configurations in which they are external to the field.Technical Note:A single 50 mA ion source cannot produce more than 3 g of separated highly enriched uranium (HEU) per year from natural abundance feed.
1B228	Hydrogen-cryogenic distillation columns having all of the following characteristics:a.Designed for operation with internal temperatures of 35 K (–238 °C) or less;b.Designed for operation at an internal pressure of 0,5 to 5 MPa;c.Constructed of either:1.Stainless steel of the 300 series with low sulphur content and with an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; or2.Equivalent materials which are both cryogenic and H2-compatible; andd.With internal diameters of 30 cm or greater and "effective lengths" of 4 m or greater.Technical Note:In 1B228 "effective length" means the active height of packing material in a packed-type column, or the active height of internal contactor plates in a plate-type column.	4.B.2.	Hydrogen-cryogenic distillation columns having all of the following characteristics:a.Designed for operation at internal temperatures of 35 K (–238 °C) or less;b.Designed for operation at internal pressures of 0,5 to 5 MPa;c.Constructed of either:1.Stainless steel of the 300 series with low sulfur content and with an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; or2.Equivalent materials which are both cryogenic and H2-compatible; andd.With internal diameters of 30 cm or greater and "effective lengths" of 4 m or greater.Technical Note:The term "effective length" means the active height of packing material in a packed-type column, or the active height of internal contactor plates in a plate-type column.
1B229	Water-hydrogen sulphide exchange tray columns and "internal contactors", as follows:N.B.:For columns which are specially designed or prepared for the production of heavy water see 0B004.a.Water-hydrogen sulphide exchange tray columns, having all of the following characteristics:1.Can operate at pressures of 2 MPa or greater;2.Constructed of carbon steel having an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; and3.With a diameter of 1,8 m or greater;b."Internal contactors" for the water-hydrogen sulphide exchange tray columns specified in 1B229.a.Technical Note:"Internal contactors" of the columns are segmented trays which have an effective assembled diameter of 1,8 m or greater, are designed to facilitate countercurrent contacting and are constructed of stainless steels with a carbon content of 0,03 % or less. These may be sieve trays, valve trays, bubble cap trays, or turbogrid trays.	4.B.1.	Water-hydrogen sulfide exchange tray columns and internal contactors, as follows:N.B.:For columns which are especially designed or prepared for the production of heavy water, see INFCIRC/254/Part 1 (as amended).a.Water-hydrogen sulfide exchange tray columns, having all of the following characteristics:1.Can operate at pressures of 2 MPa or greater;2.Constructed of carbon steel having an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; and3.With a diameter of 1,8 m or greater;b.Internal contactors for the water-hydrogen sulfide exchange tray columns specified in Item 4.B.1.a.Technical Note:Internal contactors of the columns are segmented trays which have an effective assembled diameter of 1,8 m or greater; are designed to facilitate countercurrent contacting and are constructed of stainless steels with a carbon content of 0,03 % or less. These may be sieve trays, valve trays, bubble cap trays or turbogrid trays.
1B230	Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH2/NH3), having all of the following characteristics:a.Airtight (i.e., hermetically sealed);b.A capacity greater than 8,5 m3/h; andc.Either of the following characteristics:1.For concentrated potassium amide solutions (1 % or greater), an operating pressure of 1,5 to 60 MPa; or2.For dilute potassium amide solutions (less than 1 %), an operating pressure of 20 to 60 MPa.	4.A.2.	Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH2/NH3), having all of the following characteristics:a.Airtight (i.e., hermetically sealed);b.A capacity greater than 8,5 m3/h; andc.Either of the following characteristics:1.For concentrated potassium amide solutions (1 % or greater), an operating pressure of 1,5 to 60 MPa; or2.For dilute potassium amide solutions (less than 1 %), an operating pressure of 20 to 60 MPa.
1B231	Tritium facilities or plants, and equipment therefor, as follows:a.Facilities or plants for the production, recovery, extraction, concentration, or handling of tritium;b.Equipment for tritium facilities or plants, as follows:1.Hydrogen or helium refrigeration units capable of cooling to 23 K (–250 °C) or less, with heat removal capacity greater than 150 W;2.Hydrogen isotope storage or purification systems using metal hydrides as the storage or purification medium.	2.B.1.	Tritium facilities or plants, and equipment therefor, as follows:a.Facilities or plants for the production, recovery, extraction, concentration or handling of tritium;b.Equipment for tritium facilities or plants, as follows:1.Hydrogen or helium refrigeration units capable of cooling to 23 K (–250 °C) or less, with heat removal capacity greater than 150 W;2.Hydrogen isotope storage or purification systems using metal hydrides as the storage or purification medium.
1B232	Turboexpanders or turboexpander-compressor sets having both of the following characteristics:a.Designed for operation with an outlet temperature of 35 K (–238 °C) or less; andb.Designed for a throughput of hydrogen gas of 1000 kg/h or greater.	4.A.3.	Turboexpanders or turboexpander-compressor sets having both of the following characteristics:a.Designed for operation with an outlet temperature of 35 K (– 238 °C) or less; andb.Designed for a throughput of hydrogen gas of 1000 kg/h or greater.
1B233	Lithium isotope separation facilities or plants, and systems and equipment therefor, as follows:a.Facilities or plants for the separation of lithium isotopes;b.Equipment for the separation of lithium isotopes based on the lithium-mercury amalgam process, as follows:1.Packed liquid-liquid exchange columns specially designed for lithium amalgams;2.Mercury or lithium amalgam pumps;3.Lithium amalgam electrolysis cells;4.Evaporators for concentrated lithium hydroxide solution;c.Ion exchange systems specially designed for lithium isotope separation, and specially designed components therefor;d.Chemical exchange systems (employing crown ethers, cryptands, or lariat ethers), specially designed for lithium isotope separation, and specially designed components therefor.	2.B.2.	Lithium isotope separation facilities or plants, and systems and equipment therefor, as follows:N.B.:Certain lithium isotope separation equipment and components for the plasma separation process (PSP) are also directly applicable to uranium isotope separation and are controlled under INFCIRC/254 Part 1 (as amended).a.Facilities or plants for the separation of lithium isotopes;b.Equipment for the separation of lithium isotopes based on the lithium-mercury amalgam process, as follows:1.Packed liquid-liquid exchange columns specially designed for lithium amalgams;2.Mercury or lithium amalgam pumps;3.Lithium amalgam electrolysis cells;4.Evaporators for concentrated lithium hydroxide solution;c.Ion exchange systems specially designed for lithium isotope separation, and specially designed component parts therefor;d.Chemical exchange systems (employing crown ethers, cryptands, or lariat ethers) specially designed for lithium isotope separation, and specially designed component parts therefor.
1B234	High explosive containment vessels, chambers, containers and other similar containment devices designed for the testing of high explosives or explosive devices and having both of the following characteristics:N.B.:SEE ALSO MILITARY GOODS CONTROLS.a.Designed to fully contain an explosion equivalent to 2 kg of TNT or greater; andb.Having design elements or features enabling real time or delayed transfer of diagnostic or measurement information.	5.B.7.	High explosive containment vessels, chambers, containers and other similar containment devices designed for the testing of high explosives or explosive devices and having both of the following characteristics:a.Designed to fully contain an explosion equivalent to 2 kg of TNT or greater; andb.Having design elements or features enabling real time or delayed transfer of diagnostic or measurement information.

1CMaterials

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
1C202	Alloys, other than those specified in 1C002.b.3. or .b.4., as follows:a.Aluminium alloys having both of the following characteristics:1."Capable of" an ultimate tensile strength of 460 MPa or more at 293 K (20 °C); and2.In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm;	2.C.1.	Aluminium alloys having both of the following characteristics:a."Capable of" an ultimate tensile strength of 460 MPa or more at 293 K (20 °C);b.and b. In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mmTechnical Note:In Item 2.C.1. the phrase "capable of" encompasses aluminium alloys before or after heat treatment.
1C202	b.Titanium alloys having both of the following characteristics:1."Capable of" an ultimate tensile strength of 900 MPa or more at 293 K (20 °C); and2.In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm.Technical Note:The phrase alloys "capable of" encompasses alloys before or after heat treatment.	2.C.13.	Titanium alloys having both of the following characteristics:a."Capable of" an ultimate tensile strength of 900 MPa or more at 293 K (20 °C);In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm.Technical Note:In Item 2.C.13. the phrase "capable of" encompasses titanium alloys before or after heat treatment
1C210	"Fibrous or filamentary materials" or prepregs, other than those specified in 1C010.a., b. or e., as follows:a.Carbon or aramid "fibrous or filamentary materials" having either of the following characteristics:1.A "specific modulus" of 12,7 × 106 m or greater; or2.A "specific tensile strength" of 23,5 × 104 m or greater;Note:1C210.a. does not control aramid "fibrous or filamentary materials" having 0,25 % by weight or more of an ester based fibre surface modifier;	2.C.7.a	"Fibrous or filamentary materials", and prepregs, as follows:a.Carbon or aramid "fibrous or filamentary materials" having either of the following characteristics:1.A "specific modulus" of 12,7 × 106 m or greater; or2.A "specific tensile strength" of 23,5 × 104 m or greater;Note:Item 2.C.7.a. does not control aramid "fibrous or filamentary materials" having 0,25 % or more by weight of an ester based fiber surface modifier.
	b.Glass "fibrous or filamentary materials" having both of the following characteristics:1.A "specific modulus" of 3,18 × 106 m or greater; and2.A "specific tensile strength" of 7,62 × 104 m or greater;	2.C.7.b	Glass "fibrous or filamentary materials" having both of the following characteristics:1.A "specific modulus" of 3,18 × 106 m or greater; and2.A "specific tensile strength" of 7,62 × 104 m or greater;
	c.Thermoset resin impregnated continuous "yarns", "rovings", "tows" or "tapes" with a width of 15 mm or less (prepregs), made from carbon or glass "fibrous or filamentary materials" specified in 1C210.a. or b.Technical Note:The resin forms the matrix of the composite.Note:In 1C210, "fibrous or filamentary materials" is restricted to continuous "monofilaments", "yarns", "rovings", "tows" or "tapes".	2.C.7.c	c.Thermoset resin impregnated continuous "yarns", "rovings", "tows" or "tapes" with a width of 15 mm or less (prepregs), made from carbon or glass "fibrous or filamentary materials" specified in Item 2.C.7.a. or Item 2.C.7.b.Technical Note:The resin forms the matrix of the composite.Technical Notes:1.In Item 2.C.7. "Specific modulus" is the Young's modulus in N/m2 divided by the specific weight in N/m3 when measured at a temperature of 296 ± 2 K (23 ± 2 °C) and a relative humidity of 50 ± 5 %.2.In Item 2.C.7. "Specific tensile strength" is the ultimate tensile strength in N/m2 divided by the specific weight in N/m3 when measured at a temperature of 296 ± 2 K (23 ± 2 °C) and a relative humidity of 50 ± 5 %.
1C216	Maraging steel, other than that specified in 1C116, "capable of" an ultimate tensile strength of 1950 MPa or more, at 293 K (20 °C).Note:1C216 does not control forms in which all linear dimensions are 75 mm or less.Technical Note:The phrase maraging steel "capable of" encompasses maraging steel before or after heat treatment.	2.C.11.	Maraging steel "capable of" an ultimate tensile strength of 1950 MPa or more at 293 K (20 °C).Note:Item 2.C.11. does not control forms in which all linear dimensions are 75 mm or less.Technical Note:In Item 2.C.11. the phrase "capable of" encompasses maraging steel before or after heat treatment.
1C225	Boron enriched in the boron-10 (10B) isotope to greater than its natural isotopic abundance, as follows: elemental boron, compounds, mixtures containing boron, manufactures thereof, waste or scrap of any of the foregoing.Note:In 1C225 mixtures containing boron include boron loaded materials.Technical Note:The natural isotopic abundance of boron-10 is approximately 18,5 weight per cent (20 atom per cent).	2.C.4.	Boron enriched in the boron-10 (10B) isotope to greater than its natural isotopic abundance, as follows: elemental boron, compounds, mixtures containing boron, manufactures thereof, waste or scrap of any of the foregoing.Note:In Item 2.C.4. mixtures containing boron include boron loaded materials.Technical Note:The natural isotopic abundance of boron-10 is approximately 18,5 weight percent (20 atom percent).
1C226	Tungsten, tungsten carbide, and alloys containing more than 90 % tungsten by weight, other than that specified by 1C117, having both of the following characteristics:a.In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 mm and 300 mm; andb.A mass greater than 20 kg.Note:1C226 does not control manufactures specially designed as weights or gamma-ray collimators.	2.C.14.	Tungsten, tungsten carbide, and alloys containing more than 90 % tungsten by weight, having both of the following characteristics:a.In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 and 300 mm; andb.A mass greater than 20 kg.Note:Item 2.C.14. does not control manufactures specially designed as weights or gamma-ray collimators.
1C227	Calcium having both of the following characteristics:a.Containing less than 1000 parts per million by weight of metallic impurities other than magnesium; andb.Containing less than 10 parts per million by weight of boron.	2.C.5.	Calcium having both of the following characteristics:a.Containing less than 1000 parts per million by weight of metallic impurities other than magnesium; andb.Containing less than 10 parts per million by weight of boron.
1C228	Magnesium having both of the following characteristics:a.Containing less than 200 parts per million by weight of metallic impurities other than calcium; andb.Containing less than 10 parts per million by weight of boron.	2.C.10.	Magnesium having both of the following characteristics:a.Containing less than 200 parts per million by weight of metallic impurities other than calcium; andb.Containing less than 10 parts per million by weight of boron.
1C229	Bismuth having both of the following characteristics:a.A purity of 99,99 % or greater by weight; andb.Containing less than 10 ppm (parts per million) by weight of silver.	2.C.3.	Bismuth having both of the following characteristics:a.A purity of 99,99 % or greater by weight; andb.Containing less than 10 ppm (parts per million) by weight of silver.
1C230	Beryllium metal, alloys containing more than 50 % beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing, other than that specified in the Military Goods Controls.N.B.:SEE ALSO MILITARY GOODS CONTROLS.Note:1C230 does not control the following:a.Metal windows for X-ray machines, or for bore-hole logging devices;b.Oxide shapes in fabricated or semi-fabricated forms specially designed for electronic component parts or as substrates for electronic circuits;c.Beryl (silicate of beryllium and aluminium) in the form of emeralds or aquamarines.	2.C.2.	Beryllium metal, alloys containing more than 50 % beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing.Note:Item 2.C.2. does not control the following:a.Metal windows for X-ray machines or for bore-hole logging devices;b.Oxide shapes in fabricated or semi-fabricated forms specially designed for electronic component parts or as substrates for electronic circuits;c.Beryl (silicate of beryllium and aluminium) in the form of emeralds or aquamarines.
1C231	Hafnium metal, alloys containing more than 60 % hafnium by weight, hafnium compounds containing more than 60 % hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing.	2.C.8.	Hafnium metal, alloys containing more than 60 % hafnium by weight, hafnium compounds containing more than 60 % hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing.
1C232	Helium-3 (3He), mixtures containing helium-3, and products or devices containing any of the foregoing.Note:1C232 does not control a product or device containing less than 1 g of helium-3.	2.C.18.	Helium-3 (3He), mixtures containing helium-3, and products or devices containing any of the foregoing.Note:Item 2.C.18. does not control a product or device containing less than 1 g of helium-3.
1C233	Lithium enriched in the lithium-6 (6Li) isotope to greater than its natural isotopic abundance, and products or devices containing enriched lithium, as follows: elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.Note:1C233 does not control thermoluminescent dosimeters.Technical Note:The natural isotopic abundance of lithium-6 is approximately 6,5 weight per cent (7,5 atom per cent).	2.C.9.	Lithium enriched in the lithium-6 (6Li) isotope to greater than its natural isotopic abundance and products or devices containing enriched lithium, as follows: elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.Note:Item 2.C.9. does not control thermoluminescent dosimeters.Technical Note:The natural isotopic abundance of lithium-6 is approximately 6,5 weight percent (7,5 atom percent).
1C234	Zirconium with a hafnium content of less than 1 part hafnium to 500 parts zirconium by weight, as follows: metal, alloys containing more than 50 % zirconium by weight, compounds, manufactures thereof, waste or scrap of any of the foregoing, other than those specified in 0A001.f.Note:1C234 does not control zirconium in the form of foil having a thickness of 0,10 mm or less.	2.C.15.	Zirconium with a hafnium content of less than 1 part hafnium to 500 parts zirconium by weight, as follows: metal, alloys containing more than 50 % zirconium by weight, compounds, manufactures thereof, waste or scrap of any of the foregoing.Note:Item 2.C.15. does not control zirconium in the form of foil having a thickness of 0,10 mm or less.
1C235	Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1000, and products or devices containing any of the foregoing.Note:1C235 does not control a product or device containing less than 1,48 × 103 GBq (40 Ci) of tritium.	2.C.17.	Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1000, and products or devices containing any of the foregoing.Note:Item 2.C.17. does not control a product or device containing less than 1,48 × 103 GBq of tritium.
1C236	"Radionuclides" appropriate for making neutron sources based on alpha-n reaction, other than those specified in 0C001 and 1C012.a., in the following forms:a.Elemental;b.Compounds having a total activity of 37 GBq/kg (1 Ci/kg) or greater;c.Mixtures having a total activity of 37 GBq/kg (1 Ci/kg) or greater;d.Products or devices containing any of the foregoing.Note:1C236 does not control a product or device containing less than 3,7 GBq (100 millicuries) of activity.Technical Note:In 1C236 "radionuclides" are any of the following:Actinium-225 (Ac-225)Actinium-227 (Ac-227)Californium-253 (Cf-253)Curium-240 (Cm-240)Curium-241 (Cm-241)Curium-242 (Cm-242)Curium-243 (Cm-243)Curium-244 (Cm-244)Einsteinium-253 (Es-253)Einsteinium-254 (Es-254)Gadolinium-148 (Gd-148)Plutonium-236 (Pu-236)Plutonium-238 (Pu-238)Polonium-208 (Po-208)Polonium-209 (Po-209)Polonium-210 (Po-210)Radium-223 (Ra-223)Thorium-227 (Th-227)Thorium-228 (Th-228)Uranium-230 (U-230)Uranium-232 (U-232)	2.C.19.	Radionuclides appropriate for making neutron sources based on alpha-n reaction:Actinium 225Curium 244Polonium 209Actinium 227Einsteinium 253Polonium 210Californium 253Einsteinium 254Radium 223Curium 240Gadolinium 148Thorium 227Curium 241Plutonium 236Thorium 228Curium 242Plutonium 238Uranium 230Curium 243Polonium 208Uranium 232In the following forms:a.Elemental;b.Compounds having a total activity of 37 GBq per kg or greater;c.Mixtures having a total activity of 37 GBq per kg or greater;d.Products or devices containing any of the foregoing.Note:Item 2.C.19. does not control a product or device containing less than 3,7 GBq of activity.
1C237	Radium 226 (226Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium 226, manufactures thereof, and products or devices containing any of the foregoing.Note:1C237 does not control the following:a.Medical applicators;b.A product or device containing less than 0,37 GBq (10 millicuries) of radium 226.	2.C.12.	Radium-226 (226Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium-226, manufactures thereof, and products or devices containing any of the foregoing.Note:Item 2.C.12. does not control the following:a.Medical applicators;b.A product or device containing less than 0,37 GBq of radium-226.
1C238	Chlorine trifluoride (ClF3).	2.C.6.	Chlorine trifluoride (ClF3).
1C239	High explosives, other than those specified in the Military Goods Controls, or substances or mixtures containing more than 2 % by weight thereof, with a crystal density greater than 1,8 g/cm3 and having a detonation velocity greater than 8000 m/s.	6.C.1.o	Any explosive with a crystal density greater than 1,8 g/cm3 and having a detonation velocity greater than 8000 m/s.
1C240	Nickel powder and porous nickel metal, other than those specified in 0C005, as follows:a.Nickel powder having both of the following characteristics:1.A nickel purity content of 99,0 % or greater by weight; and2.A mean particle size of less than 10 μm measured by American Society for Testing and Materials (ASTM) B330 standard;b.Porous nickel metal produced from materials specified in 1C240.a.Note:1C240 does not control the following:a.Filamentary nickel powders;b.Single porous nickel sheets with an area of 1000 cm2 per sheet or less.Technical Note:1C240.b. refers to porous metal formed by compacting and sintering the materials in 1C240.a. to form a metal material with fine pores interconnected throughout the structure.	2.C.16.	Nickel powder and porous nickel metal, as follows:N.B.:For nickel powders which are especially prepared for the manufacture of gaseous diffusion barriers see INFCIRC/254/Part 1 (as amended).a.Nickel powder having both of the following characteristics:1.A nickel purity content of 99,0 % or greater by weight; and2.A mean particle size of less than 10 μm measured by the ASTM B 330 standard;b.Porous nickel metal produced from materials specified in Item 2.C.16.a.Note:Item 2.C.16. does not control the following:a.Filamentary nickel powders;b.Single porous nickel metal sheets with an area of 1000 cm2 per sheet or less.Technical Note:Item 2.C.16.b. refers to porous metal formed by compacting and sintering the material in Item 2.C.16.a. to form a metal material with fine pores interconnected throughout the structure.
1C241	Rhenium, and alloys containing 90 % by weight or more rhenium; and alloys of rhenium and tungsten containing 90 % by weight or more of any combination of rhenium and tungsten, other than those specified in 1C226, having both of the following characteristics:a.In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 and 300 mm; andb.A mass greater than 20 kg.	2.C.20.	Rhenium, and alloys containing 90 % by weight or more rhenium; and alloys of rhenium and tungsten containing 90 % by weight or more of any combination of rhenium and tungsten, having both of the following characteristics:a.In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 and 300 mm; andb.A mass greater than 20 kg.

1DSoftware

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
1D001	"Software" specially designed or modified for the "development", "production" or "use" of equipment specified in 1B001 to 1B003.	1.D.2.	"software" means a collection of one or more "programs" or "microprograms" fixed in any tangible medium of expression
1D201	"Software" specially designed for the "use" of goods specified in 1B201.	1.D.3.	"software" means a collection of one or more "programs" or "microprograms" fixed in any tangible medium of expression

1ETechnology

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
1E201	"Technology" according to the General Technology Note for the "use" of goods specified in 1A002, 1A007, 1A202, 1A225 to 1A227, 1B201, 1B225 to 1B234, 1C002.b.3. or .b.4., 1C010.b., 1C202, 1C210, 1C216, 1C225 to 1C241 or 1D201.	1.E.1.	"Technology" -- means specific information required for the "development", "production", or "use" of any item contained in the List. This information may take the form of "technical data" or "technical assistance".
1E202	"Technology" according to the General Technology Note for the "development" or "production" of goods specified in 1A007, 1A202 or 1A225 to 1A227.	1.E.1.	"Technology" -- means specific information required for the "development", "production", or "use" of any item contained in the List. This information may take the form of "technical data" or "technical assistance".
1E203	"Technology" according to the General Technology Note for the "development" or "production" of goods specified in 1A007, 1A202 or 1A225 to 1A227.	1.E.1.	"Technology" -- means specific information required for the "development", "production", or "use" of any item contained in the List. This information may take the form of "technical data" or "technical assistance".

CATEGORY 2 — MATERIALS PROCESSING2ASystems, Equipment and Components

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
2A225	Crucibles made of materials resistant to liquid actinide metals, as follows:a.Crucibles having both of the following characteristics:1.A volume of between 150 cm3 and 8000 cm3; and2.Made of or coated with any of the following materials, or combination of the following materials, having an overall impurity level of 2 % or less by weight:a.Calcium fluoride (CaF2);b.Calcium zirconate (metazirconate) (CaZrO3);c.Cerium sulphide (Ce2S3);d.Erbium oxide (erbia) (Er2O3);e.Hafnium oxide (hafnia) (HfO2);f.Magnesium oxide (MgO);g.Nitrided niobium-titanium-tungsten alloy (approximately 50 % Nb, 30 % Ti, 20 % W);h.Yttrium oxide (yttria) (Y2O3); ori.Zirconium oxide (zirconia) (ZrO2);b.Crucibles having both of the following characteristics:1.A volume of between 50 cm3 and 2000 cm3; and2.Made of or lined with tantalum, having a purity of 99,9 % or greater by weight;c.Crucibles having all of the following characteristics:1.A volume of between 50 cm3 and 2000 cm3;2.Made of or lined with tantalum, having a purity of 98 % or greater by weight; and3.Coated with tantalum carbide, nitride, boride, or any combination thereof.	2.A.1	Crucibles made of materials resistant to liquid actinide metals, as follows:a.Crucibles having both of the following characteristics:1.A volume of between 150 cm3 (150 ml) and 8000 cm3 (8 l (litres)); and2.Made of or coated with any of the following materials, or combination of the following materials, having an overall impurity level of 2 % or less by weight:a.Calcium fluoride (CaF2);b.Calcium zirconate (metazirconate) (CaZrO3);c.Cerium sulfide (Ce2S3);d.Erbium oxide (erbia) (Er2O3);e.Hafnium oxide (hafnia) (HfO2);f.Magnesium oxide (MgO);g.Nitrided niobium-titanium-tungsten alloy (approximately 50 % Nb, 30 % Ti, 20 % W);h.Yttrium oxide (yttria) (Y2O3); ori.Zirconium oxide (zirconia) (ZrO2);b.Crucibles having both of the following characteristics:1.A volume of between 50 cm3 (50 ml) and 2000 cm3 (2 liters); and2.Made of or lined with tantalum, having a purity of 99,9 % or greater by weight;c.Crucibles having all of the following characteristics:1.A volume of between 50 cm3 (50 ml) and 2000 cm3 (2 liters);2.Made of or lined with tantalum, having a purity of 98 % or greater by weight; and3.Coated with tantalum carbide, nitride, boride, or any combination thereof.
2A226	Valves having all of the following characteristics:a.A "nominal size" of 5 mm or greater;b.Having a bellows seal; andc.Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60 % nickel by weight.Technical Note:For valves with different inlet and outlet diameters, the "nominal size" in 2A226 refers to the smallest diameter.	3.A.3.	Valves having all of the following characteristics:a.A nominal size of 5 mm or greater;b.Having a bellows seal; andc.Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60 % nickel by weight.Technical Note:For valves with different inlet and outlet diameter, the nominal size parameter in Item 3.A.3.a. refers to the smallest diameter.

2BTest, Inspection and Production Equipment

Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) or (2006) should consult the competent authorities of the Member State in which they are established.

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
2B001	Machine tools and any combination thereof, for removing (or cutting) metals, ceramics or "composites", which, according to the manufacturer's technical specification, can be equipped with electronic devices for "numerical control", as follows:N.B.:SEE ALSO 2B201.Note 1:2B001 does not control special purpose machine tools limited to the manufacture of gears. For such machines see 2B003.Note 2:2B001 does not control special purpose machine tools limited to the manufacture of any of the following:a.Crankshafts or camshafts;b.Tools or cutters;c.Extruder worms;d.Engraved or facetted jewellery parts; ore.Dental prostheses.Note 3:A machine tool having at least two of the three turning, milling or grinding capabilities (e.g., a turning machine with milling capability), must be evaluated against each applicable entry 2B001.a., b. or c.N.B.:For optical finishing machines, see 2B002.	1.B.2.	Machine tools, as follows, and any combination thereof, for removing or cutting metals, ceramics, or composites, which, according to the manufacturer's technical specifications, can be equipped with electronic devices for simultaneous "contouring control" in two or more axes:N.B.:For "numerical control" units controlled by their associated "software", see Item 1.D.3.
	a.Machine tools for turning having all of the following:1."Unidirectional positioning repeatability" equal to or less (better) than 1,1 μm along one or more linear axis; and2.Two or more axes which can be coordinated simultaneously for "contouring control";Note:2B001.a. does not control turning machines specially designed for producing contact lenses, having all of the following:a.Machine controller limited to using ophthalmic based software for part programming data input; andb.No vacuum chucking.b.Machine tools for milling having any of the following:1.Having all of the following:a."Unidirectional positioning repeatability" equal to or less (better) than 1,1 μm along one or more linear axis; andb.Three linear axes plus one rotary axis which can be coordinated simultaneously for "contouring control";2.Five or more axes which can be coordinated simultaneously for "contouring control" having any of the following;N.B.:"Parallel mechanism machine tools" are specified in 2B001.b.2.d.a."Unidirectional positioning repeatability" equal to or less (better) than 1,1 μm along one or more linear axis with a travel length less than 1 m;b."Unidirectional positioning repeatability" equal to or less (better) than 1,4 μm along one or more linear axis with a travel length equal to or greater than 1 m and less than 4 m;c."Unidirectional positioning repeatability" equal to or less (better) than 6,0 μm (along one or more linear axis with a travel length equal to or greater than 4 m; ord.Being a "parallel mechanism machine tool";Technical Note:A "parallel mechanism machine tool" is a machine tool having multiple rods which are linked with a platform and actuators; each of the actuators operates the respective rod simultaneously and independently.3.A "unidirectional positioning repeatability" for jig boring machines, equal to or less (better) than 1,1 μm along one or more linear axis; or4.Fly cutting machines having all of the following:a.Spindle "run-out" and "camming" less (better) than 0,0004 mm TIR; andb.Angular deviation of slide movement (yaw, pitch and roll) less (better) than 2 seconds of arc, TIR over 300 mm of travel;c.Machine tools for grinding having any of the following:1.Having all of the following:a."Unidirectional positioning repeatability" equal to or less (better) than 1,1 μm along one or more linear axis; andb.Three or more axes which can be coordinated simultaneously for "contouring control"; or2.Five or more axes which can be coordinated simultaneously for "contouring control" having any of the following:a."Unidirectional positioning repeatability" equal to or less (better) than 1,1 μm along one or more linear axis with a travel length less than 1 m;b."Unidirectional positioning repeatability" equal to or less (better) than 1,4 μm along one or more linear axis with a travel length equal to or greater than 1 m and less than 4 m; orc."Unidirectional positioning repeatability" equal to or less (better) than 6,0 μm along one or more linear axis with a travel length equal to or greater than 4 m.Note:2B001.c. does not control grinding machine as follows:a.Cylindrical external, internal, and external-internal grinding machines, having all of the following:1.Limited to cylindrical grinding; and2.Limited to a maximum workpiece capacity of 150 mm outside diameter or length.b.Machines designed specifically as jig grinders that do not have a z-axis or a waxis, with a "unidirectional positioning repeatability" less (better) than 1,1 μmc.Surface grinders.d.Electrical discharge machines (EDM) of the non-wire type which have two or more rotary axes which can be coordinated simultaneously for "contouring control";e.Machine tools for removing metals, ceramics or "composites", having all of the following:1.Removing material by means of any of the following:a.Water or other liquid jets, including those employing abrasive additives;b.Electron beam; orc."Laser" beam; and2.At least two rotary axes having all of the following:a.Can be coordinated simultaneously for "contouring control"; andb.A positioning "accuracy" of less (better) than 0,003°;f.Deep-hole-drilling machines and turning machines modified for deep-hole-drilling, having a maximum depth-of-bore capability exceeding 5 m.		a.Machine tools for turning, that have "positioning accuracies" with all compensations available better (less) than 6 μm according to ISO 230/2 (1988) along any linear axis (overall positioning) for machines capable of machining diameters greater than 35 mm;Note:Item 1.B.2.a. does not control bar machines (Swissturn), limited to machining only bar feed thru, if maximum bar diameter is equal to or less than 42 mm and there is no capability of mounting chucks. Machines may have drilling and/or milling capabilities for machining parts with diameters less than 42 mm.
2B006	Dimensional inspection or measuring systems, equipment and "electronic assemblies", as follows:	1.B.3.
2B006.b.	Linear and angular displacement measuring instruments, as follows:	1.B.3.	1.B.3.Dimensional inspection machines, instruments, or systems, as follows:
2B006.b.	1."Linear displacement" measuring instruments having any of the following:Note:Displacement measuring "laser" interferometers are only controlled in 2B006.b.1.c.Technical Note:For the purpose of 2B006.b.1. "linear displacement" means the change of distance between the measuring probe and the measured object.a.Non-contact type measuring systems with a "resolution" equal to or less (better) than 0,2 μm within a measuring range up to 0,2 mm;b.Linear Variable Differential Transformer (LVDT) systems having all of the following:1.Having any of the following:a."Linearity" equal to or less (better) than 0,1 % measured from 0 to the "full operating range", for LVDTs with a "full operating range" up to and including ± 5 mm; orb."Linearity" equal to or less (better) than 0,1 % measured from 0 to 5 mm for LVDTs with a "full operating range" greater than ± 5 mm; and2.Drift equal to or less (better) than 0,1 % per day at a standard ambient test room temperature ± 1 K;Technical Note:For the purposes of 2B006.b.1.b., "full operating range" is half of the total possible linear displacement of the LVDT. For example, LVDTs with a "full operating range" up to and including ± 5 mm can measure a total possible linear displacement of 10 mm.c.Measuring systems having all of the following:1.Containing a "laser"; and2.Maintaining, for at least 12 hours, at a temperature of 20 ± 1 °C, all of the following:a.A "resolution" over their full scale of 0,1 μm or less (better); andb.Capable of achieving a "measurement uncertainty" equal to or less (better) than (0,2 + L/2000) μm (L is the measured length in mm) at any point within a measuring range, when compensated for the refractive index of air; or	1.B.3.b.	b.Linear displacement measuring instruments, as follows:1.Non-contact type measuring systems with a "resolution" equal to or better (less) than 0,2 μm within a measuring range up to 0,2 mm;2.Linear variable differential transformer (LVDT) systems having both of the following characteristics:a.1."Linearity" equal to or less (better) than 0,1 % measured from 0 to the full operating range, for LVDTs with an operating range up to 5 mm; or2."Linearity" equal to or less (better) than 0,1 % measured from 0 to 5 mm for LVDTs with an operating range greater than 5 mm; andb.Drift equal to or better (less) than 0,1 % per day at a standard ambient test room temperature ± 1 K;3.Measuring systems having both of the following characteristics:a.Contain a laser; andb.Maintain for at least 12 hours, over a temperature range of ± 1 K around a standard temperature and a standard pressure:1.A "resolution" over their full scale of 0,1 μm or better; and2.With a "measurement uncertainty" equal to or better (less) than (0,2 + L/2000) μm (L is the measured length in millimeters);Note:Item 1.B.3.b.3. does not control measuring interferometer systems, without closed or open loop feedback, containing a laser to measure slide movement errors of machine tools, dimensional inspection machines, or similar equipment.Technical Note:In Item 1.B.3.b. "linear displacement" means the change of distance between the measuring probe and the measured object.
2B006.b.	2.Angular displacement measuring instruments having an angular position "accuracy" equal to or less (better) than 0,00025°;Note:2B006.b.2. does not control optical instruments, such as autocollimators, using collimated light (e.g., laser light) to detect angular displacement of a mirror.	1.B.3.c	c.Angular displacement measuring instruments having an "angular position deviation" equal to or better (less) than 0,00025°;Note:Item 1.B.3.c. does not control optical instruments, such as autocollimators, using collimated light (e.g., laser light) to detect angular displacement of a mirror.
2B116	Vibration test systems, equipment and components therefor, as follows:a.Vibration test systems employing feedback or closed loop techniques and incorporating a digital controller, capable of vibrating a system at an acceleration equal to or greater than 10 g rms between 20 Hz and 2 kHz while imparting forces equal to or greater than 50 kN, measured "bare table";b.Digital controllers, combined with specially designed vibration test software, with a "real-time control bandwidth" greater than 5 kHz designed for use with vibration test systems specified in 2B116.a.;Technical Note:In 2B116.b., "real-time control bandwidth" means the maximum rate at which a controller can execute complete cycles of sampling, processing data and transmitting control signals.c.Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force equal to or greater than 50 kN, measured "bare table", and usable in vibration test systems specified in 2B116.a.;d.Test piece support structures and electronic units designed to combine multiple shaker units in a system capable of providing an effective combined force equal to or greater than 50 kN, measured "bare table", and usable in vibration systems specified in 2B116.a.Technical Note:In 2B116, "bare table" means a flat table, or surface, with no fixture or fittings.	1.B.6.	Vibration test systems, equipment, and components as follows:a.Electrodynamic vibration test systems, having all of the following characteristics:1.Employing feedback or closed loop control techniques and incorporating a digital control2.unit;3.Capable of vibrating at 10 g RMS or more between 20 and 2000 Hz; and4.Capable of imparting forces of 50 kN or greater measured "bare table";b.b. Digital control units, combined with "software" specially designed for vibration testing, with a real-time bandwidth greater than 5 kHz and being designed for a system specified in Item 1.B.6.a.;c.c. Vibration thrusters (shaker units), with or without associated amplifiers, capable of impartingd.a force of 50 kN or greater measured "bare table", which are usable for the systems specified in Item 1.B.6.a.;e.d. Test piece support structures and electronic units designed to combine multiple shaker units into a complete shaker system capable of providing an effective combined force of 50 kN or greater, measured "bare table", which are usable for the systems specified in Item 1.B.6.a.Technical Note:In Item 1.B.6. "bare table" means a flat table, or surface, with no fixtures or fittings.
2B201	Machine tools and any combination thereof, other than those specified in 2B001, as follows, for removing or cutting metals, ceramics or "composites", which, according to the manufacturer's technical specification, can be equipped with electronic devices for simultaneous "contouring control" in two or more axes:Technical Notes:Stated "positioning accuracy" levels derived under the following procedures from measurements made according to ISO 230/2 (1988) or national equivalents may be used for each machine tool model if provided to, and accepted by, national authorities instead of individual machine tests. Stated "positioning accuracy" are to be derived as follows:1.Select five machines of a model to be evaluated;2.Measure the linear axis accuracies according to ISO 230/2 (1988);3.Determine the accuracy values (A) for each axis of each machine. The method of calculating the accuracy value is described in the ISO 230/2 (1988) standard;4.Determine the average accuracy value of each axis. This average value becomes the stated "positioning accuracy" of each axis for the model (Âx Ây...);5.Since Item 2B201 refers to each linear axis, there will be as many stated "positioning accuracy" values as there are linear axes;6.If any axis of a machine tool not controlled by 2B201.a., 2B201.b. or 2B201.c.. has a stated "positioning accuracy" of 6 μm or better (less) for grinding machines, and 8 μm or better (less) for milling and turning machines, both according to ISO 230/2 (1988), then the builder should be required to reaffirm the accuracy level once every eighteen months.Note 1:2B201 does not control special purpose machine tools limited to the manufacture of any of the following parts:a.Gears;b.Crankshafts or camshafts;c.Tools or cutters;d.Extruder worms.Note 2:A machine tool having at least two of the three turning, milling or grinding capabilities (e.g., a turning machine with milling capability), must be evaluated against each applicable entry 2B201.a., b. or c.	1.B.2.	1.B.2.Machine tools, as follows, and any combination thereof, for removing or cutting metals, ceramics, or composites, which, according to the manufacturer's technical specifications, can be equipped with electronic devices for simultaneous "contouring control" in two or more axes:N.B.:For "numerical control" units controlled by their associated "software", see Item 1.D.3.
2B201.	a.Machine tools for milling, having any of the following characteristics:1."Positioning accuracies" with "all compensations available" equal to or less (better) than 6 μm according to ISO 230/2 (1988) or national equivalents along any linear axis;2.Two or more contouring rotary axes; or3.Five or more axes which can be coordinated simultaneously for "contouring control";Note:2B201.a. does not control milling machines having the following characteristics:a.X-axis travel greater than 2 m; andb.Overall "positioning accuracy" on the x-axis more (worse) than 30 μm.	1.B.2.b	b.Machine tools for milling, having any of the following characteristics:1."Positioning accuracies" with all compensations available better (less) than 6 μm according to ISO 230/2 (1988) along any linear axis (overall positioning);2.Two or more contouring rotary axes; or3.Five or more axes which can be coordinated simultaneously for "contouring control".Note:Item 1.B.2.b. does not control milling machines having both of the following characteristics:1.X-axis travel greater than 2 m; and2.Overall "positioning accuracy" on the x-axis worse (more) than 30 μm according to ISO 230/2 (1988)
2B201	b.Machine tools for grinding, having any of the following characteristics:1."Positioning accuracies" with "all compensations available" equal to or less (better) than 4 μm according to ISO 230/2 (1988) or national equivalents along any linear axis;2.Two or more contouring rotary axes; or3.Five or more axes which can be coordinated simultaneously for "contouring control";Note:2B201.b. does not control grinding machines as follows:a.Cylindrical external, internal, and external-internal grinding machines having all of the following characteristics:1.Limited to a maximum workpiece capacity of 150 mm outside diameter or length; and2.Axes limited to x, z and c;b.Jig grinders that do not have a z-axis or a w-axis with an overall "positioning accuracy" less (better) than 4 μm according to ISO 230/2 (1988) or national equivalents.c.Machine tools for turning, that have "positioning accuracies" with "all compensations available" better (less) than 6 μm according to ISO 230/2 (1988) along any linear axis (overall positioning) for machines capable of machining diameters greater than 35 mm;Note:2B201.c. does not control bar machines (Swissturn), limited to machining only bar feed thru, if maximum bar diameter is equal to or less than 42 mm and there is no capability of mounting chucks. Machines may have drilling and/or milling capabilities for machining parts with diameters less than 42 mm.	1.B.2.c	c.Machine tools for grinding, having any of the following characteristics:1."Positioning accuracies" with all compensations available better (less) than 4 μm according to ISO 230/2 (1988) along any linear axis (overall positioning);2.Two or more contouring rotary axes; or3Five or more axes which can be coordinated simultaneously for "contouring control".Note:Item 1.B.2.c. does not control grinding machines as follows:1.Cylindrical external, internal, and external-internal grinding machines having all the following characteristics:a.Limited to a maximum workpiece capacity of 150 mm outside diameter or length; andb.Axes limited to x, z and c.2.Jig grinders that do not have a z-axis or a w-axis with an overall positioning accuracy less (better) than 4 microns. Positioning accuracy is according to ISO 230/2 (1988).
2B204	"Isostatic presses", other than those specified in 2B004 or 2B104, and related equipment, as follows:a."Isostatic presses" having both of the following characteristics:1.Capable of achieving a maximum working pressure of 69 MPa or greater; and2.A chamber cavity with an inside diameter in excess of 152 mm;b.Dies, moulds and controls, specially designed for "isostatic presses" specified in 2B204.a.Technical Note:In 2B204 the inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.	1.B.5.	1.B.5."Isostatic presses", and related equipment, as follows:a."Isostatic presses" having both of the following characteristics:1.Capable of achieving a maximum working pressure of 69 MPa or greater; and2.A chamber cavity with an inside diameter in excess of 152 mm;b.Dies, molds, and controls specially designed for the "isostatic presses" specified in Item 1.B.5.a.Technical Notes:1.In Item 1.B.5. "Isostatic presses" means equipment capable of pressurizing a closed cavity through various media (gas, liquid, solid particles, etc.) to create equal pressure in all directions within the cavity upon a workpiece or material.2.In Item 1.B.5. the inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.
2B206	Dimensional inspection machines, instruments or systems, other than those specified in 2B006, as follows:	1.B.3.	1.B.3.Dimensional inspection machines, instruments, or systems, as follows:
2B206.	a.Computer controlled or numerically controlled coordinate measuring machines (CMM) having either of the following characteristics:1.Having only two axes and having a maximum permissible error of length measurement along any axis (one dimensional), identified as any combination of E0x,MPE, E0y,MPE, or E0z,MPE, equal to or less (better) than (1,25 + L/1000) μm (where L is the measured length in mm) at any point within the operating range of the machine (i.e., within the length of the axis), according to ISO 10360-2(2009); or2.Three or more axes and having a three dimensional (volumetric) maximum permissible error of length measurement (E0,MPE) equal to or less (better) than (1,7 + L/800) μm (where L is the measured length in mm) at any point within the operating range of the machine (i.e., within the length of the axis), according to ISO 10360-2(2009);Technical Note:The E0,MPE of the most accurate configuration of the CMM specified according to ISO 10360-2(2009) by the manufacturer (e.g., best of the following: probe, stylus, length, motion parameters, environments) and with all compensations available shall be compared to the 1,7 + L/800 μm threshold.	1.B.3.a	a.Computer controlled or numerically controlled coordinate measuring machines (CMM) having either of the following characteristics:1.Having only two axes and having a maximum permissible error of length measurement along any axis (one dimensional), identified as any combination of E0x MPE, E0y MPE or E0zMPE, equal to or less(better) than (1,25 + L/1000) μm (where L is the measured length in mm) at any point within the operating range of the machine (i.e., within the length of the axis), according to ISO 10360-2(2009); or2.Three or more axes and having a three dimensional (volumetric) maximum permissible error of length measurement (E0, MPE equal to or less (better) than (1,7 + L/800) μm (where L is the measured length in mm) at any point within the operating range of the machine (i.e., within the length of the axis), according to ISO 10360-2(2009).Technical Note:The E0, MPE of the most accurate configuration of the CMM specified according to ISO 10360-2(2009) by the manufacturer (e.g., best of the following: probe, stylus length, motion parameters, environment) and with all compensations available shall be compared to the 1,7 + L/ 800 μm threshold.
2B206.	b.Systems for simultaneous linear-angular inspection of hemishells, having both of the following characteristics:1."Measurement uncertainty" along any linear axis equal to or less (better) than 3,5 μm per 5 mm; and2."Angular position deviation" equal to or less than 0,02°.Note 1:Machine tools that can be used as measuring machines are controlled if they meet or exceed the criteria specified for the machine tool function or the measuring machine function.Note 2:A machine specified in 2B206 is controlled if it exceeds the control threshold anywhere within its operating range.Technical Notes:All parameters of measurement values in 2B206 represent plus/minus i.e., not total band.	1.B.3.d	d.Systems for simultaneous linear-angular inspection of hemishells, having both of the following characteristics:1."Measurement uncertainty" along any linear axis equal to or better (less) than 3,5 μm per 5 mm; and2."Angular position deviation" equal to or less than 0,02°.
2B207	"Robots", "end-effectors" and control units, other than those specified in 2B007, as follows:a."Robots" or "end-effectors" specially designed to comply with national safety standards applicable to handling high explosives (for example, meeting electrical code ratings for high explosives);	1.A.3.a1	"Robots", "end-effectors" and control units as follows: a. "Robots" or "end-effectors" having either of the following characteristics: 1. Specially designed to comply with national safety standards applicable to handling high explosives (for example, meeting electrical code ratings for high explosives);
	b.Control units specially designed for any of the "robots" or "end-effectors" specified in 2B207.a.	1.A.3.b	Control units specially designed for any of the "robots" or "end-effectors" specified in Item 1.A.3.a.Note:Item 1.A.3. does not control "robots" specially designed for non-nuclear industrial applications such as automobile paint-spraying booths.Technical Notes:1."Robots" In Item 1.A.3. "robot" means a manipulation mechanism, which may be of the continuous path or of the point-to-point variety, may use "sensors", and has all of the following characteristics: (a) is multifunctional; (b) is capable of positioning or orienting material, parts, tools, or special devices through variable movements in three-dimensional space; (c) incorporates three or more closed or open loop servo-devices which may include stepping motors; and (d) has "user-accessible programmability" by means of teach/playback method or by means of an electronic computer which may be a programmable logic controller, i.e., without mechanical intervention.N.B.1:In the above definition "sensors" means detectors of a physical phenomenon, the output of which (after conversion into a signal that can be interpreted by a control unit) is able to generate "programs" or modify programmed instructions or numerical "program" data. This includes "sensors" with machine vision, infrared imaging, acoustical imaging, tactile feel, inertial position measuring, optical or acoustic ranging or force or torque measuring capabilities.N.B.2:In the above definition "user-accessible programmability" means the facility allowing a user to insert, modify or replace "programs" by means other than:(a)a physical change in wiring or interconnections; or(b)the setting of function controls including entry of parameters.N.B.3:The above definition does not include the following devices:(a)Manipulation mechanisms which are only manually/teleoperator controllable;(b)Fixed sequence manipulation mechanisms which are automated moving devices operating according to mechanically fixed programmed motions. The "program" is mechanically limited by fixed stops, such as pins or cams. The sequence of motions and the selection of paths or angles are not variable or changeable by mechanical, electronic, or electrical means;(c)Mechanically controlled variable sequence manipulation mechanisms which are automated moving devices operating according to mechanically fixed programmed motions. The "program" is mechanically limited by fixed, but adjustable, stops such as pins or cams. The sequence of motions and the selection of paths or angles are variable within the fixed "program" pattern. Variations or modifications of the "program" pattern (e.g., changes of pins or exchanges of cams) in one or more motion axes are accomplished only through mechanical operations;(d)Non-servo-controlled variable sequence manipulation mechanisms which are automated moving devices, operating according to mechanically fixed programmed motions. The "program" is variable but the sequence proceeds only by the binary signal from mechanically fixed electrical binary devices or adjustable stops;(e)Stacker cranes defined as Cartesian coordinate manipulator systems manufactured as an integral part of a vertical array of storage bins and designed to access the contents of those bins for storage or retrieval. 2. "End-effectors" In Item 1.A.3. "end-effectors" are grippers, "active tooling units", and any other tooling that is attached to the baseplate on the end of a "robot" manipulator arm.N.B.:In the above definition "active tooling units" is a device for applying motive power, process energy or sensing to the workpiece.
2B209	Flow forming machines, spin forming machines capable of flow forming functions, other than those specified in 2B009 or 2B109, and mandrels, as follows:a.Machines having both of the following characteristics:1.Three or more rollers (active or guiding); and2.Which, according to the manufacturer's technical specification, can be equipped with "numerical control" units or a computer control;b.Rotor-forming mandrels designed to form cylindrical rotors of inside diameter between 75 mm and 400 mm.Note:2B209.a. includes machines which have only a single roller designed to deform metal plus two auxiliary rollers which support the mandrel, but do not participate directly in the deformation process.	1.B.1.	Flow-forming machines, spin-forming machines capable of flow-forming functions, and mandrels, as follows:1.Machines having both of the following characteristics:a.Three or more rollers (active or guiding); andb.Which, according to the manufacturer's technical specification, can be equipped with "numerical control" units or a computer control;2.Rotor-forming mandrels designed to form cylindrical rotors of inside diameter between 75 and 400 mm.Note:Item 1.B.1.a. includes machines which have only a single roller designed to deform metal plus two auxiliary rollers which support the mandrel, but do not participate directly in the deformation process.
2B219	Centrifugal multiplane balancing machines, fixed or portable, horizontal or vertical, as follows:a.Centrifugal balancing machines designed for balancing flexible rotors having a length of 600 mm or more and having all of the following characteristics:1.Swing or journal diameter greater than 75 mm;2.Mass capability of from 0,9 to 23 kg; and3.Capable of balancing speed of revolution greater than 5000 r.p.m.;b.Centrifugal balancing machines designed for balancing hollow cylindrical rotor components and having all of the following characteristics:1.Journal diameter greater than 75 mm;2.Mass capability of from 0,9 to 23 kg;3.Capable of balancing to a residual imbalance equal to or less than 0,01 kg × mm/kg per plane; and4.Belt drive type.	3.B.3.	Centrifugal multiplane balancing machines, fixed or portable, horizontal or vertical, as follows:a.Centrifugal balancing machines designed for balancing flexible rotors having a length of 600 mm or more and having all of the following characteristics:1.Swing or journal diameter greater than 75 mm;2.Mass capability of from 0,9 to 23 kg; and3.Capable of balancing speed of revolution greater than 5000 rpm;b.Centrifugal balancing machines designed for balancing hollow cylindrical rotor components and having all of the following characteristics:1.Journal diameter greater than 75 mm;2.Mass capability of from 0,9 to 23 kg;3.Capable of balancing to a residual imbalance equal to or less than 0,010 kg × mm/kg per plane; and4.Belt drive type.
2B225	Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells, having either of the following characteristics:a.A capability of penetrating 0,6 m or more of hot cell wall (through-the-wall operation); orb.A capability of bridging over the top of a hot cell wall with a thickness of 0,6 m or more (over-the-wall operation).Technical Note:Remote manipulators provide translation of human operator actions to a remote operating arm and terminal fixture. They may be of "master/slave" type or operated by joystick or keypad.	1.A.4.	Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells, having either of the following characteristics:a.A capability of penetrating 0,6 m or more of hot cell wall (through-the-wall operation); orb.A capability of bridging over the top of a hot cell wall with a thickness of 0,6 m or more (over-the-wall operation).Technical Note:Remote manipulators provide translation of human operator actions to a remote operating arm and terminal fixture. They may be of a master/slave type or operated by joystick or keypad.
2B226	Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows:N.B:SEE ALSO 3B.a.Furnaces having all of the following characteristics:1.Capable of operation above 1123 K (850 °C);2.Induction coils 600 mm or less in diameter; and3.Designed for power inputs of 5 kW or more;b.Power supplies, with a specified power output of 5 kW or more, specially designed for furnaces specified in 2B226.a.Note:2B226.a. does not control furnaces designed for the processing of semiconductor wafers.	1.B.4.	Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows:a.Furnaces having all of the following characteristics:1.Capable of operation at temperatures above 1123 K (850 °C);2.Induction coils 600 mm or less in diameter; and3.Designed for power inputs of 5 kW or more;Note:Item 1.B.4.a. does not control furnaces designed for the processing of semiconductor wafers.b.Power supplies, with a specified output power of 5 kW or more, specially designed for furnaces specified in Item 1.B.4.a.
2B227	Vacuum or other controlled atmosphere metallurgical melting and casting furnaces and related equipment as follows:a.Arc remelt and casting furnaces having both of the following characteristics:1.Consumable electrode capacities between 1000 cm3 and 20000 cm3; and2.Capable of operating with melting temperatures above 1973 K (1700 °C);b.Electron beam melting furnaces and plasma atomization and melting furnaces, having both of the following characteristics:1.A power of 50 kW or greater; and2.Capable of operating with melting temperatures above 1473 K (1200 °C).c.Computer control and monitoring systems specially configured for any of the furnaces specified in 2B227.a. or b.	1.B.7.	Vacuum or other controlled atmosphere metallurgical melting and casting furnaces and related equipment, as follows:a.Arc remelt and casting furnaces having both of the following characteristics:1.Consumable electrode capacities between 1000 and 20000 cm3; and2.Capable of operating with melting temperatures above 1973 K (1700 °C);b.Electron beam melting furnaces and plasma atomization and melting furnaces, having both of the following characteristics:1.A power of 50 kW or greater; and2.Capable of operating with melting temperatures above 1473 K (1200 °C);c.Computer control and monitoring systems specially configured for any of the furnaces specified in Item 1.B.7.a. or 1.B.7.b.
2B228	Rotor fabrication or assembly equipment, rotor straightening equipment, bellows-forming mandrels and dies, as follows:a.Rotor assembly equipment for assembly of gas centrifuge rotor tube sections, baffles, and end caps;Note:2B228.a. includes precision mandrels, clamps, and shrink fit machines.b.Rotor straightening equipment for alignment of gas centrifuge rotor tube sections to a common axis;Technical Note:In 2B228.b. such equipment normally consists of precision measuring probes linked to a computer that subsequently controls the action of, for example, pneumatic rams used for aligning the rotor tube sections.c.Bellows-forming mandrels and dies for producing single-convolution bellows.Technical Note:In 2B228.c. the bellows have all of the following characteristics:1.Inside diameter between 75 mm and 400 mm;2.Length equal to or greater than 12,7 mm;3.Single convolution depth greater than 2 mm; and4.Made of high-strength aluminium alloys, maraging steel or high strength "fibrous or filamentary materials".	3.B.2.	Rotor fabrication or assembly equipment, rotor straightening equipment, bellows-forming mandrels and dies, as follows:a.Rotor assembly equipment for assembly of gas centrifuge rotor tube sections, baffles, and end caps;Note:Item 3.B.2.a. includes precision mandrels, clamps, and shrink fit machines.b.Rotor straightening equipment for alignment of gas centrifuge rotor tube sections to a common axis;Technical Note:In Item 3.B.2.b. such equipment normally consists of precision measuring probes linked to a computer that subsequently controls the action of, for example, pneumatic rams used for aligning the rotor tube sections.c.Bellows-forming mandrels and dies for producing single-convolution bellows.Technical Note:The bellows referred to in Item 3.B.2.c. have all of the following characteristics:1.Inside diameter between 75 and 400 mm;2.Length equal to or greater than 12,7 mm;3.Single convolution depth greater than 2 mm; and4.Made of high-strength aluminium alloys, maraging steel, or high strength "fibrous or filamentary materials".
2B230	All types of "pressure transducers" capable of measuring absolute pressures and having all of the following:a.Pressure sensing elements made of or protected by aluminium, aluminium alloy, aluminum oxide (alumina or sapphire), nickel, nickel alloy with more than 60 % nickel by weight, or fully fluorinated hydrocarbon polymers;b.Seals, if any, essential for sealing the pressure sensing element, and in direct contact with the process medium, made of or protected by aluminium, aluminium alloy, aluminum oxide (alumina or sapphire), nickel, nickel alloy with more than 60 % nickel by weight, or fully fluorinated hydrocarbon polymers; andc.Having either of the following characteristics:1.A full scale of less than 13 kPa and an "accuracy" of better than ± 1 % of full-scale; or2.A full scale of 13 kPa or greater and an "accuracy" of better than ± 130 Pa when measured at 13 kPa.Technical Notes:1.In 2B230 "pressure transducer" means a device that converts a pressure measurement into a signal.2.For the purposes of 2B230, "accuracy" includes non-linearity, hysteresis and repeatability at ambient temperature.	3.A.7.	All types of pressure transducers capable of measuring absolute pressures and having all of the following characteristics:a.Pressure sensing elements made of or protected by aluminium, aluminium alloy, aluminium oxide (alumina or sapphire), nickel, nickel alloy with more than 60 % nickel by weight, or fully fluorinated hydrocarbon polymers;b.Seals, if any, essential for sealing the pressure sensing element, and in direct contact with the process medium, made of or protected by aluminium, aluminium alloy, aluminium oxide (alumina or sapphire), nickel, nickel alloy with more than 60 % nickel by weight, or fully fluorinated hydrocarbon polymers; andc.Having either of the following characteristics:1.A full scale of less than 13 kPa and an "accuracy" of better than ± 1 % of full scale; or2.A full scale of 13 kPa or greater and an "accuracy" of better than ± 130 Pa when measuring at 13 kPa. TechnicalNotes:1.In Item 3.A.7. pressure transducers are devices that convert pressure measurements into a signal.2.In Item 3.A.7. "accuracy" includes non-linearity, hysteresis and repeatability at ambient temperature.
2B231	Vacuum pumps having all of the following characteristics:a.Input throat size equal to or greater than 380 mm;b.Pumping speed equal to or greater than 15 m3/s; andc.Capable of producing an ultimate vacuum better than 13 mPa.Technical Notes:1.The pumping speed is determined at the measurement point with nitrogen gas or air.2.The ultimate vacuum is determined at the input of the pump with the input of the pump blocked off.	3.A.8.	Vacuum pumps having all of the following characteristics:a.Input throat size equal to or greater than 380 mm;b.Pumping speed equal to or greater than 15 m3/s; andc.Capable of producing an ultimate vacuum better than 13,3 mPa.Technical Notes:1.The pumping speed is determined at the measurement point with nitrogen gas or air.2.The ultimate vacuum is determined at the input of the pump with the input of the pump blocked off.
2B232	High-velocity gun systems (propellant, gas, coil, electromagnetic, and electrothermal types, and other advanced systems) capable of accelerating projectiles to 1,5 km/s or greater.N.B.:SEE ALSO MILTARY GOODS CONTROLS.	5.B.2.	High-velocity gun systems (propellant, gas, coil, electromagnetic, and electrothermal types, and other advanced systems) capable of accelerating projectiles to 1,5 km/s or greater.Note:This item does not control guns specially designed for high velocity weapon systems.
2B233	Bellows-sealed scroll-type compressors and bellows-sealed scroll-type vacuum pumps having all of the following:N.B.:SEE ALSO 2B350.i.a.Capable of an inlet volume flow rate of 50 m3/h or greater;b.Capable of a pressure ratio of 2:1 or greater; andc.Having all surfaces that come in contact with the process gas made from any of the following materials:1.Aluminium or aluminium alloy;2.Aluminium oxide;3.Stainless steel;4.Nickel or nickel alloy;5.Phosphor bronze; or6.Fluoropolymers.	3.A.9.	Bellows-sealed scroll-type compressors and bellows-sealed scroll-type vacuum pumps having all of the following characteristics:a.Capable of an inlet volume flow rate of 50 m3/h or greater;b.Capable of a pressure ratio of 2:1 or greater; andc.Having all surfaces that come in contact with the process gas made from any of the following materials:1.Aluminium or aluminium alloy;2.Aluminium oxide;3.Stainless steel;4.Nickel or nickel alloy;5.Phosphor bronze; or6.Fluoropolymers.Technical Notes:1.In a scroll compressor or vacuum pump, crescent-shaped pockets of gas are trapped between one or more pairs of intermeshed spiral vanes, or scrolls, one of which moves while the other remains stationary. The moving scroll orbits the stationary scroll; it does not rotate. As the moving scroll orbits the stationary scroll, the gas pockets diminish in size (i.e., they are compressed) as they move toward the outlet port of the machine.2.In a bellows-sealed scroll compressor or vacuum pump, the process gas is totally isolated from the lubricated parts of the pump and from the external atmosphere by a metal bellows. One end of the bellows is attached to the moving scroll and the other end is attached to the stationary housing of the pump.3.Fluoropolymers include, but are not limited to, the following materials: a. Polytetrafluoroethylene (PTFE), b. Fluorinated Ethylene Propylene (FEP), c. Perfluoroalkoxy (PFA), d. Polychlorotrifluoroethylene (PCTFE); and e. Vinylidene fluoride-hexafluoropropylene copolymer.

2DSoftware

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
2D001	"Software", other than that specified in 2D002, as follows:a."Software" specially designed or modified for the "development" or "production" of equipment specified in 2A001 or 2B001b."Software" specially designed or modified for the "use" of equipment specified in 2A001.c., 2B001 or 2B003 to 2B009.Note:2D001 does not control part programming "software" that generates "numerical control" codes for machining various parts.	1.D.2.	"Software" specially designed or modified for the "use" of equipment specified in Item 1.A.3., 1.B.1., 1.B.3., 1.B.5., 1.B.6.a., 1.B.6.b., 1.B.6.d. or 1.B.7.Note:"Software" specially designed or modified for systems specified in Item 1.B.3.d. includes "software" for simultaneous measurements of wall thickness and contour.
2D002	"Software" for electronic devices, even when residing in an electronic device or system, enabling such devices or systems to function as a "numerical control" unit, capable of co-ordinating simultaneously more than four axes for "contouring control".Note 1:2D002 does not control "software" specially designed or modified for the operation of items not specified in Category 2.Note 2:2D002 does not control "software" for items specified in 2B002. See 2D001 and 2D003 for "software" for items specified in 2B002.Note 3:2D002 does not control "software" that is exported with, and the minimum necessary for the operation of, items not specified by Category 2.	1.D.3.	"Software" for any combination of electronic devices or system enabling such device(s) to function as a "numerical control" unit for machine tools, that is capable of controlling five or more interpolating axes that can be coordinated simultaneously for "contouring control".Notes:1."Software" is controlled whether exported separately or residing in a "numerical control" unit or any electronic device or system.2.Item 1.D.3. does not control "software" specially designed or modified by the manufacturers of the control unit or machine tool to operate a machine tool that is not specified in Item 1.B.2.
2D101	"Software" specially designed or modified for the "use" of equipment specified in 2B104, 2B105, 2B109, 2B116, 2B117 or 2B119 to 2B122.N.B.:SEE ALSO 9D004.	1.D.1.	"Software" specially designed or modified for the "use" of equipment specified in Item 1.A.3., 1.B.1., 1.B.3., 1.B.5., 1.B.6.a., 1.B.6.b., 1.B.6.d. or 1.B.7.Note:"Software" specially designed or modified for systems specified in Item 1.B.3.d. includes "software" for simultaneous measurements of wall thickness and contour.
2D201	"Software" specially designed for the "use" of equipment specified in 2B204, 2B206, 2B207, 2B209, 2B219 or 2B227.	1.D.1.	"Software" specially designed or modified for the "use" of equipment specified in Item 1.A.3., 1.B.1., 1.B.3., 1.B.5., 1.B.6.a., 1.B.6.b., 1.B.6.d. or 1.B.7.Note:"Software" specially designed or modified for systems specified in Item 1.B.3.d. includes "software" for simultaneous measurements of wall thickness and contour.
2D202	"Software" specially designed or modified for the "development", "production" or "use" of equipment specified in 2B201.Note:2D202 does not control part programming "software" that generates "numerical control" command codes but does not allow direct use of equipment for machining various parts.	1.D.2.	"Software" specially designed or modified for the "development", "production", or "use" of equipment specified in Item 1.B.2.Note:Item 1.D.2. does not control part programming "software" that generates "numerical control" command codes but does not allow direct use of equipment for machining various parts.

2ETechnology

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
2E001	"Technology" according to the General Technology Note for the "development" of equipment or "software" specified in 2A, 2B or 2D.Note:2E001 includes "technology" for the integration of probe systems into coordinate measurement machines specified in 2B006.a.	1.E.1	"Technology" according to the Technology Controls for the "development", "production" or "use" of equipment, material or "software" specified in 1.A. through 1.D.
2E002	"Technology" according to the General Technology Note for the "production" of equipment specified in 2A or 2B	1.E.1	"Technology" according to the Technology Controls for the "development", "production" or "use" of equipment, material or "software" specified in 1.A. through 1.D.
2E101	"Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 2B004, 2B009, 2B104, 2B109, 2B116, 2B119 to 2B122 or 2D101.	1.E.1	"Technology" according to the Technology Controls for the "development", "production" or "use" of equipment, material or "software" specified in 1.A. through 1.D.
2E201	"Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 2A225, 2A226, 2B001, 2B006, 2B007.b., 2B007.c., 2B008, 2B009, 2B201, 2B204, 2B206, 2B207, 2B209, 2B225 to 2B233, 2D201 or 2D202.	1.E.1	"Technology" according to the Technology Controls for the "development", "production" or "use" of equipment, material or "software" specified in 1.A. through 1.D.

CATEGORY 3 — ELECTRONICS3ASystems, Equipment and Components

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
3A201	Electronic components, other than those specified in 3A001, as follows;a.Capacitors having either of the following sets of characteristics:1.a.Voltage rating greater than 1,4 kV;b.Energy storage greater than 10 J;c.Capacitance greater than 0,5 μF; andd.Series inductance less than 50 nH; or2.a.Voltage rating greater than 750 V;b.Capacitance greater than 0,25 μF; andc.Series inductance less than 10 nH;	6.A.4.	Pulse discharge capacitors having either of the following sets of characteristics:a.1.Voltage rating greater than 1,4 kV;2.Energy storage greater than 10 J;3.Capacitance greater than 0,5 μF; and4.Series inductance less than 50 nH; orb.1.Voltage rating greater than 750 V;2.Capacitance greater than 0,25 μF; and3.Series inductance less than 10 nH.
3A201	b.Superconducting solenoidal electromagnets having all of the following characteristics:1.Capable of creating magnetic fields greater than 2 T;2.A ratio of length to inner diameter greater than 2;3.Inner diameter greater than 300 mm; and4.Magnetic field uniform to better than 1 % over the central 50 % of the inner volume;Note:3A201.b. does not control magnets specially designed for and exported "as parts of" medical nuclear magnetic resonance (NMR) imaging systems. The phrase "as part of" does not necessarily mean physical part in the same shipment; separate shipments from different sources are allowed, provided the related export documents clearly specify that the shipments are dispatched "as part of" the imaging systems.	3.A.4.	Superconducting solenoidal electromagnets having all of the following characteristics:a.Capable of creating magnetic fields greater than 2 T;b.A ratio of length to inner diameter greater than 2;c.Inner diameter greater than 300 mm; andd.Magnetic field uniform to better than 1 % over the central 50 % of the inner volume.Note:Item 3.A.4. does not control magnets specially designed for and exported as part of medical nuclear magnetic resonance (NMR) imaging systems.N.B.:As part of, does not necessarily mean physical part in the same shipment.Separate shipments from different sources are allowed, provided the related export documents clearly specify the as part of relationship.
3A201	c.Flash X-ray generators or pulsed electron accelerators having either of the following sets of characteristics:1.a.An accelerator peak electron energy of 500 keV or greater but less than 25 MeV; andb.With a "figure of merit" (K) of 0,25 or greater; or2.a.An accelerator peak electron energy of 25 MeV or greater; andb.A "peak power" greater than 50 MW.Note:3A201.c. does not control accelerators that are component parts of devices designed for purposes other than electron beam or X-ray radiation (electron microscopy, for example) nor those designed for medical purposes:Technical Notes:1.The "figure of merit" K is defined as:K = 1,7 × 103V2,65QV is the peak electron energy in million electron volts.If the accelerator beam pulse duration is less than or equal to 1 μs, then Q is the total accelerated charge in Coulombs. If the accelerator beam pulse duration is greater than 1 μs, then Q is the maximum accelerated charge in 1 μs.Q equals the integral of i with respect to t, over the lesser of 1 μs or the time duration of the beam pulse (Q = ∫ idt), where i is beam current in amperes and t is time in seconds.2."Peak power" = (peak potential in volts) × (peak beam current in amperes).3.In machines based on microwave accelerating cavities, the time duration of the beam pulse is the lesser of 1 μs or the duration of the bunched beam packet resulting from one microwave modulator pulse.4.In machines based on microwave accelerating cavities, the peak beam current is the average current in the time duration of a bunched beam packet.	5.B.1.	Flash X-ray generators or pulsed electron accelerators having either of the following sets of characteristics:a.1.An accelerator peak electron energy of 500 keV or greater but less than 25 MeV; and2.With a figure of merit (K) of 0,25 or greater; orb.1.An accelerator peak electron energy of 25 MeV or greater; and2.A peak power greater than 50 MW.Note:Item 5.B.1. does not control accelerators that are component parts of devices designed for purposes other than electron beam or X-ray radiation (electron microscopy, for example) nor those designed for medical purposes.Technical Notes:1.The figure of merit K is defined as: K = 1,7 × 103 V2,65Q. V is the peak electron energy in million electron volts. If the accelerator beam pulse duration is less than or equal to 1 μs, then Q is the total accelerated charge in Coulombs. If the accelerator beam pulse duration is greater than 1 ms, then Q is the maximum accelerated charge in 1 μs. Q equals the integral of i with respect to t, over the lesser of 1 ms or the time duration of the beam pulse (Q = ∫ idt ) where i is beam current in amperes and t is the time in seconds.2.Peak power = (peak potential in volts) × (peak beam current in amperes).3.In machines based on microwave accelerating cavities, the time duration of the beam pulse is the lesser of 1 ms or the duration of the bunched beam packet resulting from one microwave modulator pulse.4.In machines based on microwave accelerating cavities, the peak beam current is the average current in the time duration of a bunched beam packet.
3A225	Frequency changers or generators, other than those specified in 0B001.b.13., usable as a variable or fixed frequency motor drive, having all of the following characteristics:N.B. 1:"Software" specially designed to enhance or release the performance of a frequency changer or generator to meet the characteristics of 3A225 is specified in 3D225.N.B. 2:"Technology" in the form of codes or keys to enhance or release the performance of a frequency changer or generator to meet the characteristics of 3A225 is specified in 3E225.a.Multiphase output providing a power of 40 VA or greater;b.Operating at a frequency of 600 Hz or more; andc.Frequency control better (less) than 0,2 %.Note:3A225 does not control frequency changers or generators if they have hardware, "software" or "technology" constraints that limit the performance to less than that specified above, provided they meet any of the following:1.They need to be returned to the original manufacturer to make the enhancements or release the constraints;2.They require "software" as specified in 3D225 to enhance or release the performance to meet the characteristics of 3A225; or3.They require "technology" in the form of keys or codes as specified in 3E225 to enhance or release the performance to meet the characteristics of 3A225.Technical Notes:1.Frequency changers in 3A225 are also known as converters or inverters.2.Frequency changers in 3A225 may be marketed as Generators, Electronic Test Equipment, AC Power Supplies, Variable Speed Motors Drives, Variable Speed Drives (VSDs), Variable Frequency Drives (VFDs), Adjustable Frequency Drives (AFDs), or Adjustable Speed Drives (ASDs).	3.A.1.	Frequency changers or generators, usable as a variable frequency or fixed frequency motor drive, having all of the following characteristics:N.B.1:Frequency changers and generators especially designed or prepared for the gas centrifuge process are controlled under INFCIRC/254/Part 1 (as amended).N.B.2:"Software" specially designed to enhance or release the performance of frequency changers or generators to meet the characteristics below is controlled in 3.D.2 and 3.D.3.a.Multiphase output providing a power of 40 VA or greater;b.Operating at a frequency of 600 Hz or more; andc.Frequency control better (less) than 0,2 %.Notes:1.Item 3.A.1. only controls frequency changers intended for specific industrial machinery and/or consumer goods (machine tools, vehicles, etc.) if the frequency changers can meet the characteristics above when removed, and subject to General Note 3.2.For the purpose of export control, the Government will determine whether or not a particular frequency changer meets the characteristics above, taking into account hardware and software constraints.Technical Notes:1.Frequency changers in Item 3.A.1. are also known as converters or inverters.2.The characteristics specified in item 3.A.1. may be met by certain equipment marketed such as: Generators, Electronic Test Equipment, AC Power Supplies, Variable Speed Motor Drives, Variable Speed Drives (VSDs), Variable Frequency Drives (VFDs), Adjustable Frequency Drives (AFDs), or Adjustable Speed Drives (ASDs).
3A226	High-power direct current power supplies, other than those specified in 0B001.j.6., having both of the following characteristics:a.Capable of continuously producing, over a time period of 8 hours, 100 V or greater with current output of 500 A or greater; andb.Current or voltage stability better than 0,1 % over a time period of 8 hours.	3.A.5.	High-power direct current power supplies having both of the following characteristics:a.Capable of continuously producing, over a time period of 8 hours, 100 V or greater with current output of 500 A or greater; andb.Current or voltage stability better than 0,1 % over a time period of 8 hours.
3A227	High-voltage direct current power supplies, other than those specified in 0B001.j.5., having both of the following characteristics:a.Capable of continuously producing, over a time period of 8 hours, 20 kV or greater with current output of 1 A or greater; andb.Current or voltage stability better than 0,1 % over a time period of 8 hours.	3.A.6.	High-voltage direct current power supplies having both of the following characteristics:a.Capable of continuously producing, over a time period of 8 hours, 20 kV or greater with current output of 1 A or greater; andb.Current or voltage stability better than 0,1 % over a time period of 8 hours.
3A228	Switching devices, as follows:a.Cold-cathode tubes, whether gas filled or not, operating similarly to a spark gap, having all of the following characteristics:1.Containing three or more electrodes;2.Anode peak voltage rating of 2,5 kV or more;3.Anode peak current rating of 100 A or more; and4.Anode delay time of 10 μs or less;Note:3A228 includes gas krytron tubes and vacuum sprytron tubes.b.Triggered spark-gaps having both of the following characteristics:1.An anode delay time of 15 μs or less; and2.Rated for a peak current of 500 A or more;c.Modules or assemblies with a fast switching function, other than those specified in 3A001.g. or 3A001.h., having all of the following characteristics:1.Anode peak voltage rating greater than 2 kV;2.Anode peak current rating of 500 A or more; and3.Turn-on time of 1 μs or less.	6.A.3.	Switching devices as follows:a.Cold-cathode tubes, whether gas filled or not, operating similarly to a spark gap, having all of the following characteristics:1.Containing three or more electrodes;2.Anode peak voltage rating of 2,5 kV or more;3.Anode peak current rating of 100 A or more; and4.Anode delay time of 10 μs or less;Note:Item 6.A.3.a. includes gas krytron tubes and vacuum sprytron tubes.b.Triggered spark-gaps having both of the following characteristics:1.Anode delay time of 15 μs or less; and2.Rated for a peak current of 500 A or more;c.Modules or assemblies with a fast switching function having all of the following characteristics:1.Anode peak voltage rating greater than 2 kV;2.Anode peak current rating of 500 A or more; and3.Turn-on time of 1 μs or less.
3A229	High-current pulse generators as follows:N.B.:SEE ALSO MILITARY GOODS CONTROLS.a.Detonator firing sets (initiator systems, firesets), including electronically-charged, explosively-driven and optically-driven firing sets, other than those specified in 1A007.a., designed to drive multiple controlled detonators specified in 1A007.b.;b.Modular electrical pulse generators (pulsers) having all of the following characteristics:1.Designed for portable, mobile, or ruggedized-use;2.Capable of delivering their energy in less than 15 μs into loads of less than 40 ohms;3.Having an output greater than 100 A;4.No dimension greater than 30 cm;5.Weight less than 30 kg; and6.Specified for use over an extended temperature range 223 K (–50 °C) to 373 K (100 °C) or specified as suitable for aerospace applications.Note:3A229.b. includes xenon flash-lamp drivers.c.Micro-firing units having all of the following characteristics:1.No dimension greater than 35 mm;2.Voltage rating of equal to or greater than 1 kV; and3.Capacitance of equal to or greater than 100 nF.	6.A.2.	Firing sets and equivalent high-current pulse generators, as follows:a.Detonator firing sets (initiation systems, firesets), including electronically-charged, explosively-driven and optically-driven firing sets designed to drive multiple controlled detonators specified by Item 6.A.1. above;b.Modular electrical pulse generators (pulsers) having all of the following characteristics:1.Designed for portable, mobile, or ruggedized-use;2.Capable of delivering their energy in less than 15 μs into loads of less than 40 ohms;3.Having an output greater than 100 A;4.No dimension greater than 30 cm;5.Weight less than 30 kg; and6.Specified to operate over an extended temperature range of 223 to 373 K (–50 °C to 100 °C) or specified as suitable for aerospace applications.c.Micro-firing units having all of the following characteristics:1.No dimension greater than 35 mm;2.Voltage rating of equal to or greater than 1 kV; and3.Capacitance of equal to or greater than 100 nF.Note:Optically driven firing sets include both those employing laser initiation and laser charging. Explosively-driven firing sets include both explosive ferroelectric and explosive ferromagnetic firing set types. Item 6.A.2.b. includes xenon flashlamp drivers.
3A230	High-speed pulse generators, and "pulse heads" therefor, having both of the following characteristics:a.Output voltage greater than 6 V into a resistive load of less than 55 ohms, andb."Pulse transition time" less than 500 ps.Technical Notes:1.In 3A230, "pulse transition time" is defined as the time interval between 10 % and 90 % voltage amplitude.2."Pulse heads" are impulse forming networks designed to accept a voltage step function and shape it into a variety of pulse forms that can include rectangular, triangular, step, impulse, exponential, or monocycle types. "Pulse heads" can be an integral part of the pulse generator, they can be a plug-in module to the device or they can be an externally connected device.	5.B.6.	High-speed pulse generators, and pulse heads therefor, having both of the following characteristics:a.Output voltage greater than 6 V into a resistive load of less than 55 ohms; andb."Pulse transition time" less than 500 ps.Technical Notes:1.In Item 5.B.6.b. "pulse transition time" is defined as the time interval between 10 % and 90 % voltage amplitude.2.Pulse heads are impulse forming networks designed to accept a voltage step function and shape it into a variety of pulse forms that can include rectangular, triangular, step, impulse, exponential, or monocycle types. Pulse heads can be an integral part of the pulse generator, they can be a plug-in module to the device or they can be an externally connected device.
3A231	Neutron generator systems, including tubes, having both of the following characteristics:a.Designed for operation without an external vacuum system; andb.Utilizing any of the following:1.Electrostatic acceleration to induce a tritium-deuterium nuclear reaction; or2.Electrostatic acceleration to induce a deuterium-deuterium nuclear reaction and capable of an output of 3 × 109 neutrons/s or greater.	6.A.5.	Neutron generator systems, including tubes, having both of the following characteristics:a.Designed for operation without an external vacuum system; andb.1.Utilizing electrostatic acceleration to induce a tritium-deuterium nuclear reaction; or2.Utilizing electrostatic acceleration to induce a deuterium-deuterium nuclear reaction and capable of an output of 3 × 109 neutrons/s or greater.
3A232	Multipoint initiation systems, other than those specified in 1A007, as follows:N.B.:SEE ALSO MILITARY GOODS CONTROLS.N.B.:See 1A007.b. for detonators.a.Not used;b.Arrangements using single or multiple detonators designed to nearly simultaneously initiate an explosive surface over greater than 5000 mm2 from a single firing signal with an initiation timing spread over the surface of less than 2,5 μs.Note:3A232 does not control detonators using only primary explosives, such as lead azide.	6.A.1.	Detonators and multipoint initiation systems, as follows:a.Electrically driven explosive detonators, as follows:1.Exploding bridge (EB);2.Exploding bridge wire (EBW);3.Slapper;4.Exploding foil initiators (EFI);(see 3A232)b.Arrangements using single or multiple detonators designed to nearly simultaneously initiate an explosive surface over an area greater than 5000 mm2 from a single firing signal with an initiation timing spread over the surface of less than 2,5 μs.Note:Item 6.A.1. does not control detonators using only primary explosives, such as lead azide.Technical Note:In Item 6.A.1. the detonators of concern all utilize a small electrical conductor (bridge, bridge wire, or foil) that explosively vaporizes when a fast, high-current electrical pulse is passed through it. In nonslapper types, the exploding conductor starts a chemical detonation in a contacting highexplosive material such as PETN (pentaerythritoltetranitrate). In slapper detonators, the explosive vaporization of the electrical conductor drives a flyer or slapper across a gap, and the impact of the slapper on an explosive starts a chemical detonation. The slapper in some designs is driven by magnetic force. The term exploding foil detonator may refer to either an EB or a slapper-type detonator. Also, the word initiator is sometimes used in place of the word detonator.
3A233	Mass spectrometers, other than those specified in 0B002.g., capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor:a.Inductively coupled plasma mass spectrometers (ICP/MS);b.Glow discharge mass spectrometers (GDMS);c.Thermal ionization mass spectrometers (TIMS);d.Electron bombardment mass spectrometers having both of the following features:1.A molecular beam inlet system that injects a collimated beam of analyte molecules into a region of the ion source where the molecules are ionized by an electron beam; and2.One or more "cold traps" that can be cooled to a temperature of 193 K (–80 °C);e.Not used;f.Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides.Technical Notes:1.Electron bombardment mass spectrometers in 3A233.d. are also known as electron impact mass spectrometers or electron ionization mass spectrometers.2.In 3A233.d.2., a "cold trap" is a device that traps gas molecules by condensing or freezing them on cold surfaces. For the purposes of 3A233.d.2., a closed-loop gaseous helium cryogenic vacuum pump is not a "cold trap".	3.B.6.	Mass spectrometers capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor:N.B.:Mass spectrometers especially designed or prepared for analyzing on-line samples of uranium hexafluoride are controlled under INFCIRC/254/Part 1 (as amended).a.Inductively coupled plasma mass spectrometers (ICP/MS);b.Glow discharge mass spectrometers (GDMS);c.Thermal ionization mass spectrometers (TIMS);d.Electron bombardment mass spectrometers having both of the following features:1.A molecular beam inlet system that injects a collimated beam of analyte molecules into a region of the ion source where the molecules are ionized by an electron beam; and2.One or more cold traps that can be cooled to a temperature of 193 K (–80 °C) or less in order to trap analyte molecules that are not ionized by the electron beam;e.Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides.
3A234	Striplines to provide low inductance path to detonators with the following characteristics:a.Voltage rating greater than 2 kV; andbInductance of less than 20 nH.	6.A.6.	Striplines to provide low inductance path to detonators with the following characteristics:a.Voltage rating greater than 2 kV; andb.Inductance of less than 20 nH.

3DSoftware

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
3D002	"Software" specially designed for the "use" of equipment specified in 3B001.a. to f., 3B002 or 3A225	3.D.1.	"Software" specially designed for the "use" of equipment specified in Items 3.A.1., 3.B.3. or 3.B.4.
3D225	"Software" specially designed to enhance or release the performance of frequency changers or generators to meet the characteristics of 3A225.	3.D.3.	"Software" specially designed to enhance or release the performance characteristics of equipment controlled in Item 3.A.1.

3ETechnology

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
3E001	"Technology" according to the General Technology Note for the "development" or "production" of equipment or materials specified in 3A, 3B or 3C;Note 1:3E001 does not control "technology" for the "production" of equipment or components controlled by 3A003.Note 2:3E001 does not control "technology" for the "development" or "production" of integrated circuits specified in 3A001.a.3. to 3A001.a.12., having all of the following:a.Using "technology" at or above 0,130 μm; andb.Incorporating multi-layer structures with three or fewer metal layers.	3.E.1	"Technology" according to the Technology Controls for the "development", "production" or "use" of equipment, material or "software" specified in 3.A. through 3.D.
3E201	"Technology" according to the General Technology Note for the "use" of equipment specified in 3A001.e.2., 3A001.e.3., 3A001.g., 3A201, 3A225 to 3A234.	3.E.1	"Technology" according to the Technology Controls for the "development", "production" or "use" of equipment, material or "software" specified in 3.A. through 3.D.
3E225	"Technology", in the form of codes or keys, to enhance or release the performance of frequency changers or generators to meet the characteristics of 3A225.	3.E.1	"Technology" according to the Technology Controls for the "development", "production" or "use" of equipment, material or "software" specified in 3.A. through 3.D.

CATEGORY 6 — SENSORS AND LASERS6ASystems, Equipment and Components

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
6A005	"Lasers", other than those specified in 0B001.g.5. or 0B001.h.6., components and optical equipment, as follows:N.B.:SEE ALSO 6A205.Note 1:Pulsed "lasers" include those that run in a continuous wave (CW) mode with pulses superimposed.Note 2:Excimer, semiconductor, chemical, CO, CO2, and "non-repetitive pulsed" Nd:glass "lasers" are only specified in 6A005.d.Technical Note:"Non-repetitive pulsed" refers to "lasers" that produce either a single output pulse or that have a time interval between pulses exceeding one minute.Note 3:6A005 includes fibre "lasers".Note 4:The control status of "lasers" incorporating frequency conversion (i.e., wavelength change) by means other than one "laser" pumping another "laser" is determined by applying the control parameters for both the output of the source "laser" and the frequency-converted optical output.Note 5:6A005 does not control "lasers" as follows:a.Ruby with output energy below 20 J;b.Nitrogen;c.Krypton.Technical Note:In 6A005 "Wall-plug efficiency" is defined as the ratio of "laser" output power (or "average output power") to total electrical input power required to operate the "laser", including the power supply/conditioning and thermal conditioning/heat exchanger.a.Non-"tunable" continuous wave "(CW) lasers" having any of the following:1.Output wavelength less than 150 nm and output power exceeding 1 W;2.Output wavelength of 150 nm or more but not exceeding 510 nm and output power exceeding 30 W;Note:6A005.a.2. does not control Argon "lasers" having an output power equal to or less than 50 W.3.Output wavelength exceeding 510 nm but not exceeding 540 nm and any of the following:a.Single transverse mode output and output power exceeding 50 W; orb.Multiple transverse mode output and output power exceeding 150 W;4.Output wavelength exceeding 540 nm but not exceeding 800 nm and output power exceeding 30 W;5.Output wavelength exceeding 800 nm but not exceeding 975 nm and any of the following:a.Single transverse mode output and output power exceeding 50 W; orb.Multiple transverse mode output and output power exceeding 80 W;6.Output wavelength exceeding 975 nm but not exceeding 1150 nm and any of the following:a.Single transverse mode and output power exceeding 200 W; orb.Multiple transverse mode output and any of the following:1."Wall-plug efficiency" exceeding 18 % and output power exceeding 500 W; or2.Output power exceeding 2 kW;Note 1:6A005.a.6.b. does not control multiple transverse mode, industrial "lasers" with output power exceeding 2 kW and not exceeding 6 kW with a total mass greater than 1200 kg. For the purpose of this note, total mass includes all components required to operate the "laser", e.g., "laser", power supply, heat exchanger, but excludes external optics for beam conditioning and/or delivery.Note 2:6A005.a.6.b. does not control multiple transverse mode, industrial "lasers" having any of the following:a.Output power exceeding 500 W but not exceeding 1 kW and having all of the following:1.Beam Parameter Product (BPP) exceeding 0,7 mm•mrad; and2."Brightness" not exceeding 1024 W/( mm•mrad)2;b.Output power exceeding 1 kW but not exceeding 1,6 kW and having a BPP exceeding 1,25 mm•mradc.Output power exceeding 1,6 kW but not exceeding 2,5 kW and having a BPP exceeding 1,7 mm•mrad;d.Output power exceeding 2,5 kW but not exceeding 3,3 kW and having a BPP exceeding 2,5 mm•mrad;e.Output power exceeding 3,3 kW but not exceeding 4 kW and having a BPP exceeding 3,5 mm•mrad;f.Output power exceeding 4 kW but not exceeding 5 kW and having a BPP exceeding 5 mm•mrad;g.Output power exceeding 5 kW but not exceeding 6 kW and having a BPP exceeding 7,2 mm•mrad;h.Output power exceeding 6 kW but not exceeding 8 kW and having a BPP exceeding 12 mm•mrad; ori.Output power exceeding 8 kW but not exceeding 10 kW and having a BPP exceeding 24 mm•mrad.Technical Note:For the purpose of 6A005.a.6.b. Note 2.a., "brightness" is defined as the output power of the "laser" divided by the squared Beam Parameter Product (BPP), i.e., (output power)/BPP2.7.Output wavelength exceeding 1150 nm but not exceeding 1555 nm and of the following:a.Single transverse mode and output power exceeding 50 W; orb.Multiple transverse mode and output power exceeding 80 W; or8.Output wavelength exceeding 1555 nm and output power exceeding 1 W;	3.A.2	N. B.See also in correspondence to 6A205
	b.Non-"tunable" "pulsed lasers" having any of the following:1.Output wavelength less than 150 nm and any of the following:a.Output energy exceeding 50 mJ per pulse and "peak power" exceeding 1 W; orb."Average output power" exceeding 1 W;2.Output wavelength of 150 nm or more but not exceeding 510 nm and any of the following:a.Output energy exceeding 1,5 J per pulse and "peak power" exceeding 30 W; orb."Average output power" exceeding 30 W;Note:6A005.b.2.b. does not control Argon "lasers" having an "average output power" equal to or less than 50 W.3.Output wavelength exceeding 510 nm but not exceeding 540 nm and any of the following:a.Single transverse mode output and any of the following:1.Output energy exceeding 1,5 J per pulse and "peak power" exceeding 50 W; or2."Average output power" exceeding 50 W; orb.Multiple transverse mode output and any of the following:1.Output energy exceeding 1,5 J per pulse and "peak power" exceeding 150 W; or2."Average output power" exceeding 150 W;4.Output wavelength exceeding 540 nm but not exceeding 800 nm and any of the following:a."Pulse duration" less than 1 ps and any of the following:1.Output energy exceeding 0,005 J per pulse and "peak power" exceeding 5 GW; or2."Average output power" exceeding 20 W; orb."Pulse duration" equal to or exceeding 1 ps and any of the following:1.Output energy exceeding 1,5 J per pulse and "peak power" exceeding 30 W; or2."Average output power" exceeding 30 W;5.Output wavelength exceeding 800 nm but not exceeding 975 nm and any of the following:a."Pulse duration" less than 1 ps and any of the following:1.Output energy exceeding 0,005 J per pulse and "peak power" exceeding 5 GW; or2.Single transverse mode output and "average output power" exceeding 20 W;b."Pulse duration" equal to or exceeding 1 ps and not exceeding 1 μs and any of the following:1.Output energy exceeding 0,5 J per pulse and "peak power" exceeding 50 W;2.Single transverse mode output and "average output power" exceeding 20 W; or3.Multiple transverse mode output and "average output power" exceeding 50 W; orc."Pulse duration" exceeding 1 μs and any of the following:1.Output energy exceeding 2 J per pulse and "peak power" exceeding 50 W;2.Single transverse mode output and "average output power" exceeding 50 W; or3.Multiple transverse mode output and "average output power" exceeding 80 W;6.Output wavelength exceeding 975 nm but not exceeding 1150 nm and any of the following:a."Pulse duration" of less than 1 ps, and any of following:1.Output "peak power" exceeding 2 GW per pulse;2."Average output power" exceeding 10 W; or3.Output energy exceeding 0,002 J per pulse;b."Pulse duration" equal to or exceeding 1 ps and less than 1 ns and any of the following:1.Output "peak power" exceeding 5 GW per pulse;2."Average output power" exceeding 10 W; or3.Output energy exceeding 0,1 J per pulse;c."Pulse duration" equal to or exceeding 1 ns but not exceeding 1 μs, and any of the following:1.Single transverse mode output and any of the following:a."Peak power" exceeding 100 MW;b."Average output power" exceeding 20 W limited by design to a maximum pulse repetition frequency less than or equal to 1 kHz;c."Wall-plug efficiency" exceeding 12 %, "average output power" exceeding 100 W and capable of operating at a pulse repetition frequency greater than 1 kHz;d."Average output power" exceeding 150 W and capable of operating at a pulse repetition frequency greater than 1 kHz; ore.Output energy exceeding 2 J per pulse; or2.Multiple transverse mode output and any of the following:a."Peak power" exceeding 400 MW;b."Wall-plug efficiency" exceeding 18 % and "average output power" exceeding 500 W;c."Average output power" exceeding 2 kW; ord.Output energy exceeding 4 J per pulse; ord."Pulse duration" exceeding 1 μs and any of the following:1.Single transverse mode output and any of the following:a."Peak power" exceeding 500 kW;b."Wall-plug efficiency" exceeding 12 % and "average output power" exceeding 100 W; orc."Average output power" exceeding 150 W; or2.Multiple transverse mode output and any of the following:a."Peak power" exceeding 1 MW;b."Wall-plug efficiency" exceeding 18 % and "average output power" exceeding 500 W; orc."Average output power" exceeding 2 kW;7.Output wavelength exceeding 1150 nm but not exceeding 1555 nm, and any of the following:a."Pulse duration" not exceeding 1 μs and any of the following:1.Output energy exceeding 0,5 J per pulse and "peak power" exceeding 50 W;2.Single transverse mode output and "average output power" exceeding 20 W; or3.Multiple transverse mode output and "average output power" exceeding 50 W; orb."Pulse duration" exceeding 1 μs and any of the following:1.Output energy exceeding 2 J per pulse and "peak power" exceeding 50 W;2.Single transverse mode output and "average output power" exceeding 50 W; or3.Multiple transverse mode output and "average output power" exceeding 80 W; or8.Output wavelength exceeding 1555 nm and any of the following:a.Output energy exceeding 100 mJ per pulse and "peak power" exceeding 1 W; orb."Average output power" exceeding 1 W;c."Tunable" "lasers" having any of the following:1.Output wavelength less than 600 nm and any of the following:a.Output energy exceeding 50 mJ per pulse and "peak power" exceeding 1 W; orb.Average or CW output power exceeding 1 W;Note:6A005.c.1. does not control dye lasers or other liquid lasers, having a multimode output and a wavelength of 150 nm or more but not exceeding 600 nm and all of the following:1.Output energy less than 1,5 J per pulse or a "peak power" less than 20 W; and2.Average or CW output power less than 20 W.2.Output wavelength of 600 nm or more but not exceeding 1400 nm, and any of the following:a.Output energy exceeding 1 J per pulse and "peak power" exceeding 20 W; orb.Average or CW output power exceeding 20 W; or3.Output wavelength exceeding 1400 nm and any of the following:a.Output energy exceeding 50 mJ per pulse and "peak power" exceeding 1 W; orb.Average or CW output power exceeding 1 W;d.Other "lasers", not specified in 6A005.a., 6A005.b. or 6A005.c. as follows:1.Semiconductor "lasers" as follows:Note 1:6A005.d.1. includes semiconductor "lasers" having optical output connectors (e.g., fibre optic pigtails).Note 2:The control status of semiconductor "lasers" specially designed for other equipment is determined by the control status of the other equipment.a.Individual single-transverse mode semiconductor "lasers" having any of the following:1.Wavelength equal to or less than 1510 nm and average or CW output power, exceeding 1,5 W; or2.Wavelength greater than 1510 nm and average or CW output power, exceeding 500 mW;b.Individual, multiple-transverse mode semiconductor "lasers" having any of the following:1.Wavelength of less than 1400 nm and average or CW output power, exceeding 15W;2.Wavelength equal to or greater than 1400 nm and less than 1900 nm and average or CW output power, exceeding 2,5 W; or3.Wavelength equal to or greater than 1900 nm and average or CW output power, exceeding 1 W;c.Individual semiconductor "laser" "bars", having any of the following:1.Wavelength of less than 1400 nm and average or CW output power, exceeding 100 W;2.Wavelength equal to or greater than 1400 nm and less than 1900 nm and average or CW output power, exceeding 25 W; or3.Wavelength equal to or greater than 1900 nm and average or CW output power, exceeding 10 W;d.Semiconductor "laser" "stacked arrays" (two-dimensional arrays) having any of the following:1.Wavelength less than 1400 nm and having any of the following:a.Average or CW total output power less than 3 kW and having average or CW output "power density" greater than 500 W/cm2;b.Average or CW total output power equal to or exceeding 3 kW but less than or equal to 5 kW, and having average or CW output "power density" greater than 350 W/cm2;c.Average or CW total output power exceeding 5 kW;d.Peak pulsed "power density" exceeding 2500 W/cm2; ore.Spatially coherent average or CW total output power, greater than 150 W;2.Wavelength greater than or equal to 1400 nm but less than 1900 nm, and having any of the following:a.Average or CW total output power less than 250 W and average or CW output "power density" greater than 150 W/cm2;b.Average or CW total output power equal to or exceeding 250 W but less than or equal to 500 W, and having average or CW output "power density" greater than 50 W/cm2;c.Average or CW total output power exceeding 500 W;d.Peak pulsed "power density" exceeding 500 W/cm2; ore.Spatially coherent average or CW total output power, exceeding 15 W;3.Wavelength greater than or equal to 1900 nm and having any of the following:a.Average or CW output "power density" greater than 50 W/cm2;b.Average or CW output power greater than 10 W; orc.Spatially coherent average or CW total output power, exceeding 1,5 W; or4.At least one "laser" "bar" specified in 6A005.d.1.c.;Technical Note:For the purposes of 6A005.d.1.d., "power density" means the total "laser" output power divided by the emitter surface area of the "stacked array".e.Semiconductor "laser" "stacked arrays", other than those specified in 6A005.d.1.d., having all of the following:1.Specially designed or modified to be combined with other "stacked arrays" to form a larger "stacked array"; and2.Integrated connections, common for both electronics and cooling;Note 1:"Stacked arrays", formed by combining semiconductor "laser" "stacked arrays" specified by 6A005.d.1.e., that are not designed to be further combined or modified are specified by 6A005.d.1.d.Note 2:"Stacked arrays", formed by combining semiconductor "laser" "stacked arrays" specified by 6A005.d.1.e., that are designed to be further combined or modified are specified by 6A005.d.1.e.Note 3:6A005.d.1.e. does not control modular assemblies of single "bars" designed to be fabricated into end-to-end stacked linear arrays.Technical Notes:1.Semiconductor "lasers" are commonly called "laser" diodes.2.A "bar" (also called a semiconductor "laser" "bar", a "laser" diode "bar" or diode "bar") consists of multiple semiconductor "lasers" in a one-dimensional array.3.A "stacked array" consists of multiple "bars" forming a two-dimensional array of semiconductor "lasers".2.Carbon monoxide (CO) "lasers" having any of the following:a.Output energy exceeding 2 J per pulse and "peak power" exceeding 5 kW; orb.Average or CW output power exceeding 5 kW;3.Carbon dioxide (CO2) "lasers" having any of the following:a.CW output power exceeding 15 kW;b.Pulsed output with a "pulse duration" exceeding 10 μs and any of the following:1."Average output power" exceeding 10 kW; or2."Peak power" exceeding 100 kW; orc.Pulsed output with a "pulse duration" equal to or less than 10 μs and any of the following:1.Pulse energy exceeding 5 J per pulse; or2."Average output power" exceeding 2,5 kW;	3.A.2	a.Copper vapor lasers having both of the following characteristics:1.Operating at wavelengths between 500 and 600 nm; and2.An average output power equal to or greater than 30 W;
	4.Excimer "lasers" having any of the following:a.Output wavelength not exceeding 150 nm and any of the following:1.Output energy exceeding 50 mJ per pulse; or2."Average output power" exceeding 1 W;b.Output wavelength exceeding 150 nm but not exceeding 190 nm and any of the following:1.Output energy exceeding 1,5 J per pulse; or2."Average output power" exceeding 120 W;c.Output wavelength exceeding 190 nm but not exceeding 360 nm and any of the following:1.Output energy exceeding 10 J per pulse; or2."Average output power" exceeding 500 W; ord.Output wavelength exceeding 360 nm and any of the following:1.Output energy exceeding 1,5 J per pulse; or2."Average output power" exceeding 30 W;N.B.:For excimer "lasers" specially designed for lithography equipment, see 3B001.5."Chemical lasers" as follows:a.Hydrogen Fluoride (HF) "lasers";b.Deuterium Fluoride (DF) "lasers";c."Transfer lasers" as follows:1.Oxygen Iodine (O2-I) "lasers";2.Deuterium Fluoride-Carbon dioxide (DF-CO2) "lasers";6."Non-repetitive pulsed" Nd: glass "lasers" having any of the following:a."Pulse duration" not exceeding 1 μs and output energy exceeding 50 J per pulse; orb."Pulse duration" exceeding 1 μs and output energy exceeding 100 J per pulse;Note:"Non-repetitive pulsed" refers to "lasers" that produce either a single output pulse or that have a time interval between pulses exceeding one minute.e.Components as follows:1.Mirrors cooled either by "active cooling" or by heat pipe cooling;Technical Note:"Active cooling" is a cooling technique for optical components using flowing fluids within the subsurface (nominally less than 1 mm below the optical surface) of the optical component to remove heat from the optic.2.Optical mirrors or transmissive or partially transmissive optical or electro-optical components, other than fused tapered fibre combiners and Multi-Layer Dielectric gratings (MLDs), specially designed for use with specified "lasers";Note:Fibre combiners and MLDs are specified in 6A005.e.3.3.Fibre laser components as follows:a.Multimode to multimode fused tapered fibre combiners having all of the following:1.An insertion loss better (less) than or equal to 0,3 dB maintained at a rated total average or CW output power (excluding output power transmitted through the single mode core if present) exceeding 1000 W; and2.Number of input fibres equal to or greater than 3;b.Single mode to multimode fused tapered fibre combiners having all of the following:1.An insertion loss better (less) than 0,5 dB maintained at a rated total average or CW output power exceeding 4600 W;2.Number of input fibres equal to or greater than 3; and3.Having any of the following:a.A Beam Parameter Product (BPP) measured at the output not exceeding 1,5 mm mrad for a number of input fibres less than or equal to 5; orb.A BPP measured at the output not exceeding 2,5 mm mrad for a number of input fibres greater than 5;c.MLDs having all of the following:1.Designed for spectral or coherent beam combination of 5 or more fibre lasers; and2.CW Laser Induced Damage Threshold (LIDT) greater than or equal to 10 kW/cm2.f.Optical equipment as follows:N.B.:For shared aperture optical elements, capable of operating in "Super-High Power Laser" ("SHPL") applications, see the Military Goods Controls.1.Dynamic wavefront (phase) measuring equipment capable of mapping at least 50 positions on a beam wavefront and any of the following:a.Frame rates equal to or more than 100 Hz and phase discrimination of at least 5 % of the beam's wavelength; orb.Frame rates equal to or more than 1000 Hz and phase discrimination of at least 20 % of the beam's wavelength;2."Laser" diagnostic equipment capable of measuring "SHPL" system angular beam steering errors of equal to or less than 10 μrad;3.Optical equipment and components, specially designed for a phased-array "SHPL" system for coherent beam combination to an accuracy of λ/10 at the designed wavelength, or 0,1 μm, whichever is the smaller;4.Projection telescopes specially designed for use with "SHPL" systems;g."Laser acoustic detection equipment" having all of the following:1.CW laser output power equal to or exceeding 20 mW;2.Laser frequency stability equal to or better (less) than 10 MHz;3.Laser wavelengths equal to or exceeding 1000 nm but not exceeding 2000 nm;4.Optical system resolution better (less) than 1 nm; and5.Optical Signal to Noise ratio equal to or exceeding 103.Technical Note:"Laser acoustic detection equipment" is sometimes referred to as a Laser Microphone or Particle Flow Detection Microphone.	3.A.2	h.Pulsed excimer lasers (XeF, XeCl, KrF) having all of the following characteristics:1.Operating at wavelengths between 240 and 360 nm;2.A repetition rate greater than 250 Hz; and3.An average output power greater than 500 W;
6A202	Photomultiplier tubes having both of the following characteristics:a.Photocathode area of greater than 20 cm2; andb.Anode pulse rise time of less than 1 ns.	5.A.1.	Photomultiplier tubes having both of the following characteristics:a.Photocathode area of greater than 20 cm2; andb.Anode pulse rise time of less than 1 ns.
6A203	Cameras and components, other than those specified in 6A003, as follows:N.B. 1:"Software" specially designed to enhance or release the performance of a camera or imaging device to meet the characteristics of 6A203.a., 6A203.b. or 6A203.c. is specified in 6D203.N.B. 2:"Technology" in the form of codes or keys to enhance or release the performance of a camera or imaging device to meet the characteristics of 6A203.a., 6A203.b. or 6A203.c is specified in 6E203.Note:6A203.a. to 6A203.c. does not control cameras or imaging devices if they have hardware, "software" or "technology" constraints that limit the performance to less than that specified above, provided they meet any of the following:1.They need to be returned to the original manufacturer to make the enhancements or release the constraints;2.They require "software" as specified in 6D203 to enhance or release the performance to meet the characteristics of 6A203; or3.They require "technology" in the form of keys or codes as specified in 6E203 to enhance or release the performance to meet the characteristics of 6A203.	5.B.3.	High-speed cameras and imaging devices and components therefor, as follows:N.B.:"Software" specially designed to enhance or release the performance of cameras or imaging devices to meet the characteristics below is controlled in 5.D.1 and 5.D.2.
6A203	a.Streak cameras, and specially designed components therefor, as follows:1.Streak cameras with writing speeds greater than 0,5 mm/μs;2.Electronic streak cameras capable of 50 ns or less time resolution;3.Streak tubes for cameras specified in 6A203.a.2.;4.Plug-ins specially designed for use with streak cameras which have modular structures and that enable the performance specifications in 6A203.a.1. or 6A203.a.2.;5.Synchronizing electronics units, rotor assemblies consisting of turbines, mirrors and bearings specially designed for cameras specified in 6A203.a.1.;	5.B.3.a	a.Streak cameras, and specially designed components therefor, as follows:1.Streak cameras with writing speeds greater than 0,5 mm/μs;2.Electronic streak cameras capable of 50 ns or less time resolution;3.Streak tubes for cameras specified in 5.B.3.a.2.;4.Plug-ins specially designed for use with streak cameras which have modular structures and that enable the performance specifications in 5.B.3.a.1 or 5.B.3.a.2.;5.Synchronizing electronics units, rotor assemblies consisting of turbines, mirrors and bearings specially designed for cameras specified in 5.B.3.a.1.
6A203	b.Framing cameras, and specially designed components therefor, as follows:1.Framing cameras with recording rates greater than 225000 frames per second;2.Framing cameras capable of 50 ns or less frame exposure time;3.Framing tubes and solid-state imaging devices having a fast image gating (shutter) time of 50ns or less specially designed for cameras specified in 6A203.b.1 or 6A203.b.2.;4.Plug-ins specially designed for use with framing cameras which have modular structures and that enable the performance specifications in 6A203.b.1 or 6A203.b.2.;5.Synchronizing electronics units, rotor assemblies consisting of turbines, mirrors and bearings specially designed for cameras specified in 6A203.b.1 or 6A203.b.2.;Technical Note:In 6A203.b., high speed single frame cameras can be used alone to produce a single image of a dynamic event, or several such cameras can be combined in a sequentially-triggered system to produce multiple images of an event.	5.B.3.b	b.Framing cameras and specially designed components therefor as follows:1.Framing cameras with recording rates greater than 225000 frames per second;2.Framing cameras capable of 50 ns or less frame exposure time;3.Framing tubes and solid-state imaging devices having a fast image gating (shutter) time of 50ns or less specially designed for cameras specified in 5.B.3.b.1 or 5.B.3.b.2.;4.Plug-ins specially designed for use with framing cameras which have modular structures and that enable the performance specifications in 5.B.3.b.1 or 5.B.3.b.2.;5.Synchronizing electronics units, rotor assemblies consisting of turbines, mirrors and bearings specially designed for cameras specified in 5.B.3.b.1 or 5.B.3.b.2.
6A203	c.Solid state or electron tube cameras, and specially designed components therefor, as follows:1.Solid-state cameras or electron tube cameras with a fast image gating (shutter) time of 50 ns or less;2.Solid-state imaging devices and image intensifiers tubes having a fast image gating (shutter) time of 50 ns or less specially designed for cameras specified in 6A203.c.1.;3.Electro-optical shuttering devices (Kerr or Pockels cells) with a fast image gating (shutter) time of 50 ns or less;4.Plug-ins specially designed for use with cameras which have modular structures and that enable the performance specifications in 6A203.c.1.	5.B.3.c	c.Solid state or electron tube cameras and specially designed components therefor as follows:1.Solid-state cameras or electron tube cameras with a fast image gating (shutter) time of 50 ns or less;2.Solid-state imaging devices and image intensifiers tubes having a fast image gating (shutter) time of 50 ns or less specially designed for cameras specified in 5.B.3.c.1.;3.Electro-optical shuttering devices (Kerr or Pockels cells) with a fast image gating (shutter) time of 50 ns or less;4.Plug-ins specially designed for use with cameras which have modular structures and that enable the performance specifications in 5.B.3.c.1.Technical Note:High speed single frame cameras can be used alone to produce a single image of a dynamic event, or several such cameras can be combined in a sequentially-triggered system to produce multiple images of an event.
6A203	d.Radiation-hardened TV cameras, or lenses therefor, specially designed or rated as radiation hardened to withstand a total radiation dose greater than 50 × 103 Gy(silicon) (5 × 106 rad (silicon)) without operational degradation.Technical Note:The term Gy(silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionising radiation.	1.A.2.	Radiation-hardened TV cameras, or lenses therefor, specially designed or rated as radiation hardened to withstand a total radiation dose greater than 5 × 104 Gy (silicon) without operational degradation.Technical Note:The term Gy (silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionizing radiation.
6A205	"Lasers", "laser" amplifiers and oscillators, other than those specified in 0B001.g.5., 0B001.h.6. and 6A005; as follows:N.B.:For copper vapour lasers, see 6A005.b.	3.A.2.	Lasers, laser amplifiers and oscillators as follows:N.B.See also in correspondence to 6A005
6A205	a.Argon ion "lasers" having both of the following characteristics:1.Operating at wavelengths between 400 nm and 515 nm; and2.An average output power greater than 40 W;	3.A.2.b	Argon ion lasers having both of the following characteristics:1.Operating at wavelengths between 400 and 515 nm; and2.An average output power greater than 40 W;
6A205	b.Tunable pulsed single-mode dye laser oscillators having all of the following characteristics:1.Operating at wavelengths between 300 nm and 800 nm;2.An average output power greater than 1 W;3.A repetition rate greater than 1 kHz; and4.Pulse width less than 100 ns;	3.A.2.d	Tunable pulsed single-mode dye laser oscillators having all of the following characteristics:1.Operating at wavelengths between 300 and 800 nm;2.An average output power greater than 1 W;3.A repetition rate greater than 1 kHz; and4.Pulse width less than 100 ns;
6A205	c.Tunable pulsed dye laser amplifiers and oscillators, having all of the following characteristics:1.Operating at wavelengths between 300 nm and 800 nm;2.An average output power greater than 30 W;3.A repetition rate greater than 1 kHz; and4.Pulse width less than 100 ns;Note:6A205.c. does not control single mode oscillators;	3.A.2.e	Tunable pulsed dye laser amplifiers and oscillators having all of the following characteristics:1.Operating at wavelengths between 300 and 800 nm;2.An average output power greater than 30 W;3.A repetition rate greater than 1 kHz; and4.Pulse width less than 100 ns;Note:Item 3.A.2.e. does not control single mode oscillators.
6A205	d.Pulsed carbon dioxide "lasers" having all of the following characteristics:1.Operating at wavelengths between 9000 nm and 11000 nm;2.A repetition rate greater than 250 Hz;3.An average output power greater than 500 W; and4.Pulse width of less than 200 ns;	3.A.2.g	Pulsed carbon dioxide lasers having all of the following characteristics:1.Operating at wavelengths between 9000 and 11000 nm;2.A repetition rate greater than 250 Hz;3.An average output power greater than 500 W; and4.Pulse width of less than 200 ns;Note:Item 3.A.2.g. does not control the higher power (typically 1 to 5 kW) industrial CO2 lasers used in applications such as cutting and welding, as these latter lasers are either continuous wave or are pulsed with a pulse width greater than 200 ns.
6A205	e.Para-hydrogen Raman shifters designed to operate at 16 μm output wavelength and at a repetition rate greater than 250 Hz;	3.A.2.i.	Para-hydrogen Raman shifters designed to operate at 16 mm output wavelength and at a repetition rate greater than 250 Hz.
6A205	f.Neodymium-doped (other than glass) "lasers" with an output wavelength between 1000 and 1100 nm having either of the following1.Pulse-excited and Q-switched with a pulse duration equal to or more than 1 ns, and having either of the following:a.A single–transverse mode output with an average output power greater than 40 W; orb.A multiple-transverse mode output having an average power greater than 50 W; or2.Incorporating frequency doubling to give an output wavelength between 500 and 550 nm with an average output power of more than 40 W;	3.A.2.c.	Neodymium-doped (other than glass) lasers with an output wavelength between 1000 and 1100 nm having either of the following:1.Pulse-excited and Q-switched with a pulse duration equal to or greater than 1 ns, and having either of the following:a.A single-transverse mode output with an average output power greater than 40 W; orb.A multiple-transverse mode output with an average output power greater than 50 W;or2.Incorporating frequency doubling to give an output wavelength between 500 and 550 nm with an average output power of greater than 40 W;
6A205	g.Pulsed carbon monoxide lasers, other than those specified in 6A005.d.2., having all of the following:1.Operating at wavelengths between 5000 and 6000 nm;2.A repetition rate greater than 250 Hz;3.An average output power greater than 200 W; and4.Pulse width of less than 200 ns.	3.A.2.j	Pulsed carbon monoxide lasers having all of the following characteristics:1.Operating at wavelengths between 5000 and 6000 nm;2.A repetition rate greater than 250 Hz;3.An average output power greater than 200 W; and4.Pulse width of less than 200 ns;Note:Item 3.A.2.j. does not control the higher power (typically 1 to 5 kW) industrial CO lasers used in applications such as cutting and welding, as these latter lasers are either continuous wave or are pulsed with a pulse width greater than 200 ns
6A225	Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 microseconds.Note:6A225 includes velocity interferometers such as VISARs (Velocity Interferometer Systems for Any Reflector), DLIs (Doppler Laser Interferometers) and PDV (Photonic Doppler Velocimeters) also known as Het-V (Heterodyne Velocimeters).	5.B.5.a	Specialized instrumentation for hydrodynamic experiments, as follows:a.Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 ms;
6A226	Pressure sensors, as follows:a.Shock pressure gauges capable of measuring pressures greater than 10 GPa, including gauges made with manganin, ytterbium, and polyvinylidene bifluoride (PVBF, PVF2);b.Quartz pressure transducers for pressures greater than 10 GPa.	5.B.5.b.	b.Shock pressure gauges capable of measuring pressures greater than 10 GPa, including gauges made with manganin, ytterbium, and polyvinylidene bifluoride (PVBF, PVF2);
		5.B.5.c.	c.Quartz pressure transducers for pressures greater than 10 GPa.Note:Item 5.B.5.a. includes velocity interferometers such as VISARs (Velocity Interferometer Systems for Any Reflector), DLIs (Doppler Laser Interferometers) and PDV (Photonic Doppler Velocimeters) also known as Het-V (Heterodyne Velocimeters).

6DSoftware

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
6D203	"Software" specially designed to enhance or release the performance of cameras or imaging devices to meet the characteristics of 6A203.a. to 6A203.c.	5.D.2.	"Software" or encryption keys/codes specially designed to enhance or release the performance characteristics of equipment controlled in Item 5.B.3.

6ETechnology

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.9/Part 2
6E201	"Technology" according to the General Technology Note for the "use" of equipment specified in 6A003, 6A005.a.2., 6A005.b.2., 6A005.b.3., 6A005.b.4., 6A005.b.6., 6A005.c.2., 6A005.d.3.c., 6A005.d.4.c., 6A202, 6A203, 6A205, 6A225 or 6A226.	5.D.1.	"Technology" according to the Technology Controls for the "development", "production" or "use" of equipment, material or "software" specified in 5.A. through 5.D.
6E203	"Technology", in the form of codes or keys, to enhance or release the performance of cameras or imaging devices to meet the characteristics of 6A203a. to 6A203.c.	5.D.1.	"Technology" according to the Technology Controls for the "development", "production" or "use" of equipment, material or "software" specified in 5.A. through 5.D.

ANNEX IIList of other goods and technology, including software, referred to in Article 3aINTRODUCTORY NOTES1.Unless otherwise stated, reference numbers used in the column entitled "Description" refer to the descriptions of dual-use items set out in Annex I to Regulation (EC) No 428/2009.2.A reference number in the column entitled "Related item from Annex I to Regulation (EC) No 428/2009" means that the characteristics of the item described in the column "Description" lie outside the parameters set out in the description of the dual-use entry referred to.3.Definitions of terms between "single quotation marks" are given in a technical note to the relevant item.4.Definitions of terms between "double quotation marks" can be found in Annex I to Regulation (EC) No 428/2009.GENERAL NOTES1.The object of the controls contained in this Annex should not be defeated by the export of any non-controlled goods (including plant) containing one or more controlled components when the controlled component or components are the principal element of the goods and can feasibly be removed or used for other purposes.N.B.:In judging whether the controlled component or components are to be considered the principal element, it is necessary to weigh the factors of quantity, value and technological know-how involved and other special circumstances which might establish the controlled component or components as the principal element of the goods being procured.2.The goods specified in this Annex include both new and used goods.GENERAL TECHNOLOGY NOTE (GTN)(To be read in conjunction with section II.B.)1.The sale, supply, transfer or export of "technology" which is "required" for the "development", "production" or "use" of goods the sale, supply, transfer or export of which is controlled in Part A (Goods) below, is controlled in accordance with the provisions of Section II.B.2.The "technology" "required" for the "development", "production" or "use" of goods under control remains under control even when applicable to non-controlled goods.3.Controls do not apply to that "technology" which is the minimum necessary for the installation, operation, maintenance (checking) and repair of those goods which are not controlled or the export of which has been authorised in accordance with Regulation (EC) No 423/2007 or this Regulation.4.Controls on "technology" transfer do not apply to information "in the public domain", to "basic scientific research" or to the minimum necessary information for patent applications.II.A.GOODS

A0.Nuclear Materials, Facilities, and Equipment
No	Description	Related item from Annex I to Regulation (EC) No 428/2009
II.A0.001	Hollow cathode lamps as follows:a.Iodine hollow cathode lamps with windows in pure silicon or quartzb.Uranium hollow cathode lamps	—
II.A0.002	Faraday isolators in the wavelength range 500 nm – 650 nm	—
II.A0.003	Optical gratings in the wavelength range 500 nm – 650 nm	—
II.A0.004	Optical fibres in the wavelength range 500 nm – 650 nm coated with anti-reflecting layers in the wavelength range 500 nm – 650 nm and having a core diameter greater than 0,4 mm but not exceeding 2 mm	—
II.A0.005	Nuclear reactor vessel components and testing equipment, other than those specified in 0A001, as follows:1.Seals2.Internal components3.Sealing, testing and measurement equipment	0A001
II.A0.006	Nuclear detection systems for detection, identification or quantification of radioactive materials and radiation of nuclear origin and specially designed components thereof other than those specified in 0A001.j. or 1A004.c.	0A001.j1A004.c
II.A0.007	Bellows-sealed valves made of aluminium alloy or stainless steel type 304, 304L or 316L.Note:This item does not cover bellow valves defined in 0B001.c.6 and 2A226.	0B001.c.62A226
II.A0.008	Laser mirrors, other than those specified in 6A005.e, consisting of substrates having a thermal expansion coefficient of 10– 6 K– 1 or less at 20 °C (e.g. fused silica or sapphire).Note:This item does not cover optical systems specially designed for astronomical applications, except if the mirrors contain fused silica.	0B001.g.5, 6A005.e
II.A0.009	Laser lenses, other than those specified in 6A005.e.2, consisting of substrates having a thermal expansion coefficient of 10– 6 K– 1 or less at 20 °C (e.g. fused silica).	0B001.g, 6A005.e.2
II.A0.010	Pipes, piping, flanges, fittings made of, or lined with, nickel or nickel alloy containing more than 40 % nickel by weight, other than those specified in 2B350.h.1.	2B350
II.A0.011	Vacuum pumps other than those specified in 0B002.f.2 or 2B231, as follows:Turbomolecular pumps having a flowrate equal to or greater than 400 l/s,Roots type vacuum roughing pumps having a volumetric aspiration flowrate greater than 200 m3/h.Bellows-sealed, scroll, dry compressor, and bellows-sealed, scroll, dry vacuum pumps.	0B002.f.2, 2B231
II.A0.012	Shielded enclosures for the manipulation, storage and handling of radioactive substances (Hot cells).	0B006
II.A0.013	"Natural uranium" or "depleted uranium" or thorium in the form of metal, alloy, chemical compound or concentrate and any other material containing one or more of the foregoing, other than those specified in 0C001.	0C001
II.A0.014	Detonation chambers having a capacity of explosion absorption of more than 2.5 kg TNT equivalent.	—
II.A0.015	"Glove Boxes", specially designed for radioactive isotopes, radioactive sources or radionuclides.Technical Note:"Glove Boxes" means equipment providing protection to the user, from hazardous vapour, particles or radiation, from materials inside the equipment being handled or processed by a person outside the equipment, by means of manipulators or gloves integrated into the equipment.	0B006
II.A0.016	Toxic gas monitoring systems designed for continuous operation and detection of Hydrogen Sulphide, and specially designed detectors therefore.	0A0010B001.c
II.A0.017	Helium Leak Detectors.	0A0010B001.c
A1.aterials, chemicals, "microorganisms" and "toxins"
No	Description	Related item from Annex I to Regulation (EC) No 428/2009
II.A1.001	Bis(2-ethylhexyl) phosphoric acid (HDEHP or D2HPA) CAS 298-07-7 solvent in any quantity, with a purity greater than 90 %.	—
II.A1.002	Fluorine gas (Chemical Abstract Number (CAS): 7782-41-4), with a purity of at least 95 %.	—
II.A1.003	Ring-shaped seals and gaskets, having an inner diameter of 400 mm or less, made of any of the following materials:a.Copolymers of vinylidene fluoride having 75 % or more beta crystalline structure without stretching;b.Fluorinated polyimides containing 10 % by weight or more of combined fluorine;c.Fluorinated phosphazene elastomers containing 30 % by weight or more of combined fluorine;d.Polychlorotrifluoroethylene (PCTFE, e.g. Kel-F ®);e.Fluoro-elastomers (e.g., Viton ®, Tecnoflon ®);f.Polytetrafluoroethylene (PTFE).	—
II.A1.004	Personal equipment for detecting radiation of nuclear origin, including personal dosimeters.Note:This item does not cover nuclear detection systems defined in item 1A004.c.	1A004.c
II.A1.005	Electrolytic cells for fluorine production with an output capacity greater than 100 g of fluorine per hour.Note:This item does not cover electrolytic cells defined in item 1B225.	1B225
II.A1.006	Catalysts, other than those prohibited by 1A225, containing platinum, palladium or rhodium, usable for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water.	1B231, 1A225
II.A1.007	Aluminium and its alloys, other than those specified in 1C002.b.4 or 1C202.a, in crude or semi-fabricated form having either of the following characteristics:a.Capable of an ultimate tensile strength of 460 MPa or more at 293 K (20 °C); orb.Having a tensile strength of 415 MPa or more at 298 K (25 °C).	1C002.b.4, 1C202.a
II.A1.008	Magnetic metals, of all types and of whatever form, having an initial relative permeability of 120000 or more and a thickness between 0,05 and 0,1 mm.	1C003.a
II.A1.009	"Fibrous or filamentary materials" or prepregs, as follows:N.B.SEE ALSO II.A1.019.A.a.Carbon or aramid "fibrous or filamentary materials" having either of the following characteristics:1.A "specific modulus" exceeding 10 × 106 m; or2.A "specific tensile strength" exceeding 17 × 104 m;b.Glass "fibrous or filamentary materials" having either of the following characteristics:1.A "specific modulus" exceeding 3,18 × 106 m; or2.A "specific tensile strength" exceeding 76,2 × 103 m;c.Thermoset resin-impregnated continuous "yarns", "rovings", "tows" or "tapes" with a width of 15 mm or less (once prepregs), made from carbon or glass "fibrous or filamentary materials" other than those specified in II.A1.010.a. or b.Note:This item does not cover "fibrous or filamentary materials" defined in items 1C010.a, 1C010.b, 1C210.a and 1C210.b.	1C010.a1C010.b1C210.a1C210.b
II.A1.010	Resin-impregnated or pitch-impregnated fibres (prepregs), metal or carbon-coated fibres (preforms) or "carbon fibre preforms", as follows:a.Made from "fibrous or filamentary materials" specified in II.A1.009 above;b.Epoxy resin "matrix" impregnated carbon "fibrous or filamentary materials" (prepregs), specified in 1C010.a, 1C010.b or 1C010.c, for the repair of aircraft structures or laminates, of which the size of individual sheets does not exceed 50 cm × 90 cm;c.Prepregs specified in 1C010.a, 1C010.b or 1C010.c, when impregnated with phenolic or epoxy resins having a glass transition temperature (Tg) less than 433 K (160 °C) and a cure temperature lower than the glass transition temperature.Note:This item does not cover "fibrous or filamentary materials" defined in item 1C010.e.	1C010.e.1C210
II.A1.011	Reinforced silicon carbide ceramic composites usable for nose tips, re-entry vehicles, nozzle flaps, usable in "missiles", other than those specified in 1C107.	1C107
II.A1.012	Maraging steels, other than those specified in 1C116 or 1C216, "capable of" an ultimate tensile strength of 2050 MPa or more, at 293 K (20 °C).Technical Note:The phrase "maraging steel capable of" encompasses maraging steel before or after heat treatment.	1C216
II.A1.013	Tungsten, tantalum, tungsten carbide, tantalum carbide and alloys, having both of the following characteristics:a.In forms having a hollow cylindrical or spherical symmetry (including cylinder segments) with an inside diameter between 50 mm and 300 mm; andb.A mass greater than 5 kg.Note:This item does not cover tungsten, tungsten carbide and alloys defined in item 1C226.	1C226
II.A1.014	Elemental powders of cobalt, neodymium or samarium or alloys or mixtures thereof containing at least 20 % by weight of cobalt, neodymium or samarium, with a particle size less than 200 μm.	—
II.A1.015	Pure tributyl phosphate (TBP) [CAS No 126-73-8] or any mixture having a TBP content of more than 5 % by weight.	—
II.A1.016	Maraging steel, other than those prohibited by 1C116, 1C216 or II.A1.012Technical Note:Maraging steels are iron alloys generally characterised by high nickel, very low carbon content and the use of substitutional elements or precipitates to produce strengthening and age-hardening of the alloy.	—
II.A1.017	Metals, metal powders and material as follows:a.Tungsten and tungsten alloys, other than those prohibited by 1C117, in the form of uniform spherical or atomized particles of 500 μm diameter or less with a tungsten content of 97 % by weight or more;b.Molybdenum and molybdenum alloys, other than those prohibited by 1C117, in the form of uniform spherical or atomized particles of 500 μm diameter or less with a molybdenum content of 97 % by weight or more;c.Tungsten materials in the solid form, other than those prohibited by 1C226, or II.A1.013 having material compositions as follows:1.Tungsten and alloys containing 97 % by weight or more of tungsten;2.Copper infiltrated tungsten containing 80 % by weight or more of tungsten; or3.Silver infiltrated tungsten containing 80 % by weight or more of tungsten.	—
II.A1.018	Soft magnetic alloys having a chemical composition as follows:(a)Iron content between 30 % and 60 %, and(b)Cobalt content between 40 % and 60 %.	—
II.A1.019	"Fibrous or filamentary materials" or prepregs, not prohibited by Annex I or by Annex II (under II.A1.009, II.A1.010) of this Regulation, or not specified by Annex I of Regulation (EC) No 428/2009, as follows:(a)Carbon "fibrous or filamentary materials";Note:II.A1.019a. does not cover fabrics.(b)Thermoset resin-impregnated continuous "yarns", "rovings", "tows", or "tapes", made from carbon "fibrous or filamentary materials";(c)Polyacrylonitrile (PAN) continuous "yarns", "rovings", "tows" or "tapes"	—
II.A1.020	Steel alloys in sheet or plate form, having any of the following characteristics:(a)Steel alloys "capable of" ultimate tensile strength of 1200 MPa or more, at 293 K (20 °C); or(b)Nitrogen-stabilised duplex stainless steel.Note:The phrase alloys "capable of" encompasses alloys before or after heat treatmentTechnical Note:"Nitrogen-stabilised duplex stainless steel" has a two-phase microstructure consisting of grains of ferritic and austenitic steel with the addition of nitrogen to stabilise the microstructure.	1C1161C216
II.A1.021	Carbon-Carbon Composite material.	1A002.b.1
II.A1.022	Nickel alloys in crude or semi-fabricated form, containing 60 % by weight or more nickel.	1C002.c.1.a
II.A1.023	Titanium alloys in sheet or plate form "capable of" an ultimate tensile strength of 900 MPa or more at 293 K (20 °C).Note:The phrase alloys "capable of" encompasses alloys before or after heat treatment.	1C002.b.3
II.A1.024	Propellants and constituent chemicals for propellants as follows:(a)Toluene Diisocyanate (TDI)(b)Methyl Diphenyl Diisocyanate (MDI)(c)Isophorone Diiscocyanate (IPDI)(d)Sodium Perchlorate(e)Xylidine(f)Hydroxy Terminated Polyether (HTPE)(g)Hydroxy Terminated Caprolactone Ether (HTCE)Technical Note:This item refers to pure substance and any mixture containing at least 50 % of one of the chemicals mentioned above.	1C111
II.A1.025	"Lubricating materials" containing, as their principal ingredients, any of the following:(a)Perfluoroalkylether, (CAS 60164-51-4);(b)Perfluoropolyalkylether, PFPE, (CAS 6991-67-9)."Lubricating materials" means oils and fluids.	1C006
II.A1.026	Beryllium-Copper or Copper-Beryllium Alloys in plate, sheet, strip or rolled bar form, having a composition comprising Copper as the major element by weight and other elements including less than 2 % by weight Beryllium.	1C002.b
A2.Materials Processing
No	Description	Related item from Annex I to Regulation (EC) No 428/2009
II.A2.001	Vibration test systems, equipment and components thereof, other than those specified in 2B116:a.Vibration test systems employing feedback or closed loop techniques and incorporating a digital controller, capable of vibrating a system at an acceleration equal to or greater than 0,1 g rms between 0,1 Hz and 2 kHz and imparting forces equal to or greater than 50 kN, measured "bare table";b.Digital controllers, combined with specially designed vibration test "software", with a real-time bandwidth greater than 5 kHz designed for use with vibration test systems specified in a.;c.Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force equal to or greater than 50 kN, measured "bare table", and usable in vibration test systems specified in a.;d.Test piece support structures and electronic units designed to combine multiple shaker units in a system capable of providing an effective combined force equal to or greater than 50 kN, measured "bare table", and usable in vibration systems specified in a.Technical Note:"Bare table" means a flat table, or surface, with no fixture or fittings.	2B116
II.A2.002	Machine tools and components and numerical controls for machine tools, as follows:a.Machine tools for grinding having positioning accuracies with "all compensations available" equal to or less (better) than 15 μm according to ISO 230/2 (1988) (1) or national equivalents along any linear axis;Note:This item does not cover machine tools for grinding defined in items 2B201.b and 2B001.c.b.Components and numerical controls, specially designed for machine tools specified in 2B001, 2B201, or under a.	2B201.b2B001.c
II.A2.003	Balancing machines and related equipment as follows:a.Balancing machines, designed or modified for dental or other medical equipment, having all the following characteristics:1.Not capable of balancing rotors/assemblies having a mass greater than 3 kg;2.Capable of balancing rotors/assemblies at speeds greater than 12500 rpm;3.Capable of correcting imbalance in two planes or more; and4.Capable of balancing to a residual specific imbalance of 0,2 g × mm per kg of rotor mass;b.Indicator heads designed or modified for use with machines specified in a. above.Technical Note:Indicator heads are sometimes known as balancing instrumentation.	2B119
II.A2.004	Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells, other than those specified in 2B225, having either of the following characteristics:a.A capability of penetrating a hot cell wall of 0,3 m or more (through the wall operation); orb.A capability of bridging over the top of a hot cell wall with a thickness of 0,3 m or more (over the wall operation).	2B225
II.A2.006	Furnaces capable of operation at temperatures above 400 °C as follows:a.Oxidation furnacesb.Controlled atmosphere heat treatment furnacesNote:This item does not cover tunnel kilns with roller or car conveyance, tunnel kilns with conveyor belt, pusher type kilns or shuttle kilns, specially designed for the production of glass, tableware ceramics or structural ceramics.	2B2262B227
II.A2.007	"Pressure transducers", other than those defined in 2B230, capable of measuring absolute pressures at any point in the range 0 to 200 kPa and having both of the following characteristics:a.Pressure sensing elements made of or protected by "Materials resistant to corrosion by uranium hexafluoride (UF6)", andb.Having either of the following characteristics:1.A full scale of less than 200 kPa and an "accuracy" of better than ± 1 % of full scale; or2.A full scale of 200 kPa or greater and an "accuracy" of better than 2 kPa.	2B230
II.A2.008	Liquid-liquid contacting equipment (mixer-settlers, pulsed columns, centrifugal contactors); and liquid distributors, vapour distributors or liquid collectors designed for such equipment, where all surfaces that come in direct contact with the chemical(s) being processed are made from the following materials:N.B.SEE ALSO II.A2.0141.Stainless steel.Note:for stainless steel with more than 25 % nickel and 20 % chromium by weight see entry II.A2.014.a	2B350.e
II.A2.009	Industrial equipment and components, other than those specified in 2B350.d, as follows:N.B.SEE ALSO II.A2.015Heat exchangers or condensers with a heat transfer surface area greater than 0,05 m2, and less than 30 m2; and tubes, plates, coils or blocks (cores) designed for such heat exchangers or condensers, where all surfaces that come in direct contact with the fluid(s) are made from the following materials:1.Stainless steel.Note 1:for stainless steel with more than 25 % nickel and 20 % chromium by weight see entry II.A2.015aNote 2:This item does not cover vehicle radiators.Technical Note:The materials used for gaskets and seals and other implementation of sealing functions do not determine the status of control of the heat exchanger.	2B350.d
II.A2.010	Multiple-seal, and seal-less pumps, other than those specified in 2B350.i, suitable for corrosive fluids, with manufacturer's specified maximum flow-rate greater than 0,6 m3/hour, or vacuum pumps with manufacturer's specified maximum flow-rate greater than 5 m3/hour [measured under standard temperature (273 K or 0 °C) and pressure (101,3 kPa) conditions]; and casings (pump bodies), preformed casing liners, impellers, rotors or jet pump nozzles designed for such pumps, in which all surfaces that come in direct contact with the chemical(s) being processed are made from the following materials:N.B.SEE ALSO II.A2.0161.Stainless steel;Note:for stainless steel with more than 25 % nickel and 20 % chromium by weight see entry II.A2.016aTechnical Note:The materials used for gaskets and seals and other implementation of sealing functions do not determine the status of control of the pump.	2B350.i
II.A2.011	Centrifugal separators, capable of continuous separation without the propagation of aerosols and manufactured from:1.Alloys with more than 25 % nickel and 20 % chromium by weight;2.Fluoropolymers;3.Glass (including vitrified or enamelled coating or glass lining);4.Nickel or alloys with more than 40 % nickel by weight;5.Tantalum or tantalum alloys;6.Titanium or titanium alloys; or7.Zirconium or zirconium alloys.Note:This item does not cover centrifugal separators defined in item 2B352.c.	2B352.c
II.A2.012	Sintered metal filters made of nickel or nickel alloy with more than 40 % nickel by weight.Note:This item does not cover filters defined in item 2B352.d.	2B352.d
II.A2.013	Spin-forming machines and flow-forming machines, other than those controlled by 2B009, 2B109 or 2B209, having a roller force of more than 60 kN and specially designed components therefor.Technical Note:For the purpose of II.A2.013, machines combining the functions of spin-forming and flow-forming are regarded as flow-forming machines.	—
II.A2.014	Liquid-liquid contacting equipment (mixer-settlers, pulsed columns, centrifugal contactors); and liquid distributors, vapour distributors or liquid collectors designed for such equipment where all surfaces that come in direct contact with the chemical(s) being processed are any of the following:N.B.SEE ALSO II.A2.008.a.Made from any of the following materials:1.Alloys with more than 25 % nickel and 20 % chromium by weight;2.Fluoropolymers;3.Glass (including vitrified or enamelled coating or glass lining);4.Graphite or "carbon graphite";5.Nickel or alloys with more than 40 % nickel by weight;6.Tantalum or tantalum alloys;7.Titanium or titanium alloys; or8.Zirconium or zirconium alloys; orb.Made from both stainless steel and one or more of the materials specified in II.A2.014.a.Technical Note:"Carbon graphite" is a composition consisting of amorphous carbon and graphite, in which the graphite content is 8 % or more by weight.	2B350.e
II.A2.015	Industrial equipment and components, other than those specified in 2B350.d, as follows:N.B.SEE ALSO II.A2.009.Heat exchangers or condensers with a heat transfer surface area greater than 0,05 m2, and less than 30 m2; and tubes, plates, coils or blocks (cores) designed for such heat exchangers or condensers, where all surfaces that come in direct contact with the fluid(s) are any of the following:a.Made from any of the following materials:1.Alloys with more than 25 % nickel and 20 % chromium by weight;2.Fluoropolymers;3.Glass (including vitrified or enamelled coating or glass lining);4.Graphite or "carbon graphite";5.Nickel or alloys with more than 40 % nickel by weight;6.Tantalum or tantalum alloys;7.Titanium or titanium alloys;8.Zirconium or zirconium alloys;9.Silicon carbide; or10.Titanium carbide; orb.Made from both stainless steel and one or more of the materials specified in II.A2.015.a.Note:This item does not cover vehicle radiators.Technical Note:The materials used for gaskets and seals and other implementation of sealing functions do not determine the status of control of the heat exchanger.	2B350.d
II.A2.016	Multiple-seal, and seal-less pumps, other than those specified in 2B350.i, suitable for corrosive fluids, with manufacturer's specified maximum flow-rate greater than 0,6 m3/hour, or vacuum pumps with manufacturer's specified maximum flow-rate greater than 5 m3/hour [measured under standard temperature (273 K or 0 °C) and pressure (101,3 kPa) conditions]; and casings (pump bodies), preformed casing liners, impellers, rotors or jet pump nozzles designed for such pumps, in which all surfaces that come in direct contact with the chemical(s) being processed are any of the following:NB.SEE ALSO II.A2.010.a.Made from any of the following materials:1.Alloys with more than 25 % nickel and 20 % chromium by weight;2.Ceramics;3.Ferrosilicon;4.Fluoropolymers;5.Glass (including vitrified or enamelled coatings or glass lining);6.Graphite or "carbon graphite"7.Nickel or alloys with more than 40 % nickel by weight;8.Tantalum or tantalum alloys;9.Titanium or titanium alloys;10.Zirconium or zirconium alloys;11.Niobium (columbium) or niobium alloys; or12.Aluminium alloys; orb.Made from both stainless steel and one or more of the materials specified in II.A2.016.a.Technical Note:The materials used for gaskets and seals and other implementation of sealing functions do not determine the status of control of the pump.	2B350.i
II.A2.017	Electrical Discharge Machine (EDM) tools for removing or cutting metals, ceramics or "composites", as follows, and specially designed ram, sinker or wire electrodes therefor:(a)Ram or sinker electrode Electrical Discharge Machines;(b)Wire electrode Electrical Discharge Machines.Note:Electrical Discharge Machines are also known as Spark Erosion Machines or Wire Erosion Machines.	2B001.d
II.A2.018	Computer controlled or "numerically controlled" co-ordinate measuring machines (CMM), or dimensional inspection machines, having a three dimensional (volumetric) maximum permissible error of indication (MPPE) at any point in the operating range of the machine (i.e. within the length axes) equal to or less (better) than (3 + L/1000) μm (L is the measured length in mm), tested according to ISO 10360-2 (2001), and measurement probes designed therefor.	2B006.a2B206.a
II.A2.019	Computer controlled or "numerically controlled" Electron Beam Welding Machines, and specially designed components therefor.	2B001.e.1.b
II.A2.020	Computer controlled or "numerically controlled" Laser Welding and Laser Cutting Machines, and specially designed components therefor.	2B001.e.1.c
II.A2.021	Computer controlled or "numerically controlled" Plasma Cutting Machines, and specially designed components therefor.	2B001.e.1
II.A2.022	Vibration Monitoring Equipment specially designed for rotors or rotating equipment and machinery, capable of measuring any frequency in the range 600-2000 Hz.	2B116
II.A2.023	Liquid Ring Vacuum Pumps, and specially designed components therefore.	2B2312B350.i
II.A2.024	Rotary Vane Vacuum Pumps, and specially designed components therefore.Note 1:II.A2.024 does not control rotary vane vacuum pumps that are specially designed for specific other equipment.Note 2:The control status of rotary vane vacuum pumps that are specially designed for specific other equipment is determined by the control status of the other equipment	2B2312B235.i0B002.f
II.A2.025	Air filters, as follows, having one or more physical size dimension exceeding 1000 mm:(a)High Efficiency Particulate Air (HEPA) filters;(b)Ultra-Low Penetration Air (ULPA) filters.Note:II.A2.025 does not control air filters specially designed for medical equipment.	2B352.d
A3.Electronics
No	Description	Related item from Annex I to Regulation (EC) No 428/2009
II.A3.001	High voltage direct current power supplies having both of the following characteristics:a.Capable of continuously producing, over a time period of eight hours, 10 kV or more, with output power of 5 kW or more with or without sweeping; andb.Current or voltage stability better than 0,1 % over a time period of four hours.Note:This item does not cover power supplies defined in items 0B001.j.5 and 3A227.	3A227
II.A3.002	Mass spectrometers, other than those specified in 3A233 or 0B002.g, capable of measuring ions of 200 atomic mass units or more and having a resolution of better than 2 parts in 200, as follows, and ion sources thereof:a.Inductively coupled plasma mass spectrometers (ICP/MS);b.Glow discharge mass spectrometers (GDMS);c.Thermal ionisation mass spectrometers (TIMS);d.Electron bombardment mass spectrometers which have a source chamber constructed from, lined with or plated with "materials resistant to corrosion by uranium hexafluoride UF6";e.Molecular beam mass spectrometers having either of the following characteristics:1.A source chamber constructed from, lined with or plated with stainless steel or molybdenum and equipped with a cold trap capable of cooling to 193 K (– 80 °C) or less; or2.A source chamber constructed from, lined with or plated with "materials resistant to corrosion by uranium hexafluoride (UF6)";f.Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides.	3A233
II.A3.003	Spectrometers and diffractometers, designed for the indicative test or quantitative analysis of the elemental composition of metals or alloys without chemical decomposition of the material.	—
II.A3.004	Frequency changers or generators, and Variable Speed electrical drives, other than those prohibited by 0B001 or 3A225, having all of the following characteristics, and specially designed components and software therefor:a.Multiphase output capable of providing a power of 10 W or greater;b.Capable of operating at a frequency of 600 Hz or more; andc.Frequency control better (less) than 0,2 %.Technical Note:Frequency changers are also known as converters or inverters.Notes:1.Item II.A3.004 does not control frequency changers that include communication protocols or interfaces designed for specific industrial machinery (such as machine tools, spinning machines, printed circuit board machines) so that the frequency changers cannot be used for other purposes while meeting the performance characteristics above.2.Item II.A3.004 does not control frequency changers specially designed for vehicles and which operate with a control sequence that is mutually communicated between the frequency changer and the vehicle control unit.	3A2250B001.b.13
A6.Sensors and Lasers
No	Description	Related item from Annex I to Regulation (EC) No 428/2009
II.A6.001	Yttrium aluminium garnet (YAG) rods	—
II.A6.002	Optical equipment and components, other than those specified in 6A002, 6A004.b as follows:Infrared optics in the wavelength range 9000 nm – 17000 nm and components thereof, including cadmium telluride (CdTe) components.	6A0026A004.b
II.A6.003	Wave front corrector systems for use with a laser beam having a diameter exceeding 4 mm, and specially designed components thereof, including control systems, phase front sensors and "deformable mirrors" including bimorph mirrors.Note:This item does not cover mirrors defined in 6A004.a, 6A005.e and 6A005.f.	6A003
II.A6.004	Argon ion "lasers" having an average output power equal to or greater than 5 W.Note:This item does not cover argon ion "lasers" defined in items 0B001.g.5, 6A005 and 6A205.a.	6A005.a.66A205.a
II.A6.005	Semiconductor "lasers" and components thereof, as follows:a.Individual semiconductor "lasers" with an output power greater than 200 mW each, in quantities larger than 100;b.Semiconductor "laser" arrays having an output power greater than 20 W.Notes:1.Semiconductor "lasers" are commonly called "laser" diodes.2.This item does not cover "lasers" defined in items 0B001.g.5, 0B001.h.6 and 6A005.b.3.This item does not cover "laser" diodes with a wavelength in the range 1200 nm – 2000 nm.	6A005.b
II.A6.006	Tunable semiconductor "lasers" and tunable semiconductor "laser" arrays, of a wavelength between 9 μm and 17 μm, as well as array stacks of semiconductor "lasers" containing at least one tunable semiconductor "laser" array of such wavelength.Notes:1.Semiconductor "lasers" are commonly called "laser" diodes.2.This item does not cover semiconductor "lasers" defined in items 0B001.h.6 and 6A005.b	6A005.b
II.A6.007	Solid state "tunable" "lasers" and specially designed components thereof as follows:a.Titanium-sapphire lasers,b.Alexandrite lasers.Note:This item does not cover titanium-sapphire and alexandrite lasers defined in items 0B001.g.5, 0B001.h.6 and 6A005.c.1.	6A005.c.1
II.A6.008	Neodymium-doped (other than glass) "lasers", having an output wavelength greater than 1000 nm but not exceeding 1100 nm and output energy exceeding 10 J per pulse.Note:This item does not cover neodymium-doped (other than glass) "lasers" defined in item 6A005.c.2.b.	6A005.c.2
II.A6.009	Components of acousto-optics, as follows:a.Framing tubes and solid-state imaging devices having a recurrence frequency equal to or exceeding 1 kHz;b.Recurrence frequency supplies;c.Pockels cells.	6A203.b.4.c
II.A6.010	Radiation-hardened cameras, or lenses thereof, other than those specified in 6A203.c., specially designed, or rated as radiation-hardened, to withstand a total radiation dose greater than 50 × 103 Gy (silicon) (5 × 106 rad (silicon)) without operational degradation.Technical Note:The term Gy(silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionising radiation.	6A203.c
II.A6.011	Tunable pulsed dye laser amplifiers and oscillators, having all of the following characteristics:1.Operating at wavelengths between 300 nm and 800 nm;2.An average output power greater than 10 W but not exceeding 30 W;3.A repetition rate greater than 1 kHz; and4.Pulse width less than 100 ns.Notes:1.This item does not cover single mode oscillators.2.This item does not cover tunable pulsed dye laser amplifiers and oscillators defined in item 6A205.c, 0B001.g.5 and 6A005.	6A205.c
II.A6.012	Pulsed carbon dioxide "lasers" having all of the following characteristics:1.Operating at wavelengths between 9000 nm and 11000 nm;2.A repetition rate greater than 250 Hz;3.An average output power greater than 100 W but not exceeding 500 W; and4.Pulse width less than 200 ns.Note:This item does not cover pulsed carbon dioxide laser amplifiers and oscillators defined in item 6A205.d., 0B001.h.6. and 6A005.d.	6A205.d
II.A6.013	Copper vapour "lasers" having both of the following characteristics:1.Operating at wavelengths between 500 and 600 nm; and2.An average output power equal to or greater than 15 W.	6A005.b
II.A6.014	Pulsed carbon monoxide "lasers" having all of the following characteristics:1.Operating at wavelengths between 5000 and 6000 nm;2.A repetition rate greater than 250 Hz;3.An average output power greater than 100 W; and4.Pulse width of less than 200 ns.Note:This item does not control the higher power (typically 1 to 5 kW) industrial carbon monoxide lasers used in applications such as cutting and welding, as these latter lasers are either continuous wave or are pulsed with a pulse width greater than 200 ns.
II.A6.015	"Vacuum pressure gauges", being electrically powered and having measurement accuracy of 5 % or less (better)."Vacuum pressure gauges" include Pirani Gauges, Penning Gauges and Capacitance Manometers.	0B001.b
II.A6.016	Microscopes and related equipment and detectors, as follows:(a)Scanning Electron Microscopes;(b)Scanning Auger Microscopes;(c)Transmission Electron Microscopes;(d)Atomic Force Microscopes;(e)Scanning Force Microscopes;(f)Equipment and detectors, specially designed for use with the microscopes specified in II.A6.013 a) to e) above, employing any of the following materials analysis techniques:1.X-ray Photo Spectroscopy (XPS);2.Energy-dispersive X-ray Spectroscopy (EDX, EDS); or3.Electron Spectroscopy for Chemical Analysis (ESCA).	6B
A7.Navigation and Avionics
No	Description	Related item from Annex I to Regulation (EC) No 428/2009
II.A7.001	Inertial navigation systems and specially designed components thereof, as follows:I.Inertial navigation systems which are certified for use on "civil aircraft" by civil authorities of a State participating in the Wassenaar Arrangement, and specially designed components thereof, as follows:a.Inertial navigation systems (INS) (gimballed or strapdown) and inertial equipment designed for "aircraft", land vehicle, vessels (surface or underwater) or "spacecraft" for attitude, guidance or control, having any of the following characteristics, and specially designed components thereof:1.Navigation error (free inertial) subsequent to normal alignment of 0,8 nautical mile per hour (nm/hr) "Circular Error Probable" (CEP) or less (better); or2.Specified to function at linear acceleration levels exceeding 10 g;b.Hybrid Inertial Navigation Systems embedded with Global Navigation Satellite Systems(s) (GNSS) or with "Data-Based Referenced Navigation" ("DBRN") System(s) for attitude, guidance or control, subsequent to normal alignment, having an INS navigation position accuracy, after loss of GNSS or "DBRN" for a period of up to four minutes, of less (better) than 10 metres "Circular Error Probable" (CEP);c.Inertial Equipment for Azimuth, Heading, or North Pointing having any of the following characteristics, and specially designed components thereof:1.Designed to have an Azimuth, Heading, or North Pointing accuracy equal to, or less (better) than 6 arc/ minutes RMS at 45 degrees latitude; or2.Designed to have a non-operating shock level of at least 900 g at a duration of at least 1 msec.Note:The parameters of I.a. and I.b. are applicable with any of the following environmental conditions:1.Input random vibration with an overall magnitude of 7,7 g rms in the first half hour and a total test duration of one and a half hours per axis in each of the three perpendicular axes, when the random vibration meets the following:a.A constant power spectral density (PSD) value of 0,04 g2/Hz over a frequency interval of 15 to 1000 Hz; andb.The PSD attenuates with a frequency from 0,04 g2/Hz to 0,01 g2/Hz over a frequency interval from 1000 to 2000 Hz;2.A roll and yaw rate equal to or greater than + 2,62 radian/s (150 deg/s); or3.According to national standards equivalent to 1. or 2. above.Technical Notes:1.I.b. refers to systems in which an INS and other independent navigation aids are built into a single unit (embedded) in order to achieve improved performance.2."Circular Error Probable" (CEP) — In a circular normal distribution, the radius of the circle containing 50 percent of the individual measurements being made, or the radius of the circle within which there is a 50 percent probability of being located.II.Theodolite systems incorporating inertial equipment specially designed for civil surveying purposes and designed to have an Azimuth, Heading, or North Pointing accuracy equal to, or less (better) than 6 arc minutes RMS at 45 degrees latitude, and specially designed components thereof.III.Inertial or other equipment using accelerometers specified in 7A001 or 7A101, where such accelerometers are specially designed and developed as MWD (Measurement While Drilling) sensors for use in downhole well services operations.	7A0037A103
II.A7.002	Accelerometers containing piezoelectric ceramic transducer element, having a sensitivity of 1000 mV/g or better (higher)	7A001
A9.Aerospace and Propulsion
No	Description	Related item from Annex I to Regulation (EC) No 428/2009
II.A9.001	Explosive bolts.	—
II.A9.002	"Load Cells" capable of measuring rocket motor thrust having a capacity exceeding 30 kN.Technical Note:"Load Cells" means devices and transducers for the measurement of force in both tension and in compression.Note:II.A9.002 does not include equipment, devices or transducers, specially designed for the measurement of the weight of vehicles, e.g. weigh bridges.	9B117
II.A9.003	Electrical power generation gas turbines, components and related equipment as follows:(a)Gas Turbines specially designed for electrical power generation, having an output exceeding 200 MW;(b)Vanes, Stators, Combustion Chambers and Fuel Injection Nozzles, specially designed for electrical power generation gas turbines specified in II.A9.003.a;(c)Equipment specially designed for the "development" and "production" of electrical power generation gas turbines specified in II. A9.003.a.	9A0019A0029A0039B0019B0039B004

II.B.TECHNOLOGY

No	Description	Related item from Annex I to Regulation (EC) No 428/2009
II.B.001	Technology required for the development, production, or use of the items in Part II.A. (Goods) above.Technical Note:The term "technology" includes software.	—

ANNEX IIAEnd-use statement referred to in Articles 3a(6) and 3c(2) and point (b) of Article 3d(2)(Letterhead of the end-user/consignee in the country of final destination)END-USE STATEMENT(if issued by the governmental authority, please insert a unique identifying number "No…")A.PARTIES1.Exporter (name, address and contact details)2.Consignee (name, address and contact details)3.End-user (if different from consignee)4.Country of final destinationB.ITEMS1.Items (detailed description of items)2.Quantity (units) / weight3.End-use (specific purpose for which the items will be used. If the items are to be incorporated into or used for the development, production, use or repair of another item, please describe that item, its purpose and its end-user)4.Specification of the end-use location of the items (unless the consignee acts as trader, wholeseller or reseller and is not aware of the end-use location of the items)C.STATEMENT OF FOREIGN CONSIGNEEC.1Consignee acts as end-userArticles 3a(6) and 3c(2) and point (b) of Article 3d(2) of Council Regulation (EU) No 267/2012 require the applicant for an authorisation to submit this end-use statement or an equivalent document containing information on the end-use and end-use location of any supplied item.We (I) state that the items described in Section B supplied by the exporter named in Section A 1:1.will only be used for the purposes described in Section B 3 and that the items or any replica thereof, if applicable, are intended for final use in the country named in Section A 4, in the location specified in Section B 4;2.that the items or any replica thereof, if applicable:will not be used in any nuclear explosive activity or unsafeguarded nuclear fuel-cycle activity;will not be used for any purpose connected with chemical or biological or nuclear weapons, or missiles capable of delivering such weapons;will only be used for civil end-uses;will not be retransferred within Iran without prior information to the exporting State.C.2Consignee acts as trader, wholeseller or reseller (only to be completed if Section C.1 is not applicable)Articles 3a(6) and 3c(2) and point (b) of Article 3d(2) of Council Regulation (EU) No 267/2012 require the applicant for an authorisation to submit this end-use statement or an equivalent document containing information on the end-use and end-use location of any supplied item.We (I) state that the items described in Section B supplied by the exporter named in Section A 1:1.will only be used for the purposes described in Section B 3 and that the items or any replica thereof, if applicable, are intended for final use in the country named in Section A 42.that the items or any replica thereof, if applicable:will not be used in any nuclear explosive activity or unsafeguarded nuclear fuel-cycle activity;will not be used for any purpose connected with chemical or biological or nuclear weapons, or missiles capable of delivering such weapons;will only be used for civil end-uses;will only be delivered to a third person/company on condition that that third person/company accepts the commitments of the above declaration as binding for itself and on condition that that third person/company is known to be trustworthy and reliable in the observance of such commitments.

SIGNATURE
…Place, date	…Original signature of end-user/consignee
…Company stamp/official seal	…Name and title of signer in block letters

If applicable:Stamp of chamber of commerce(or other legalising authority)ANNEX IIICATEGORY 1 — SPECIAL MATERIALS AND RELATED EQUIPMENT1ASystems, Equipment and Components

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
1A002	"Composite" structures or laminates, having any of the following:a.Consisting of an organic "matrix" and materials specified in 1C010.c., 1C010.d. or 1C010.e.; orb.Consisting of a metal or carbon "matrix", and any of the following:1.Carbon "fibrous or filamentary materials" having all of the following:a.A "specific modulus" exceeding 10,15 × 106 m; andb.A "specific tensile strength" exceeding 17,7 × 104 m; or2.Materials specified in 1C010.c.Note 1:1A002 does not control composite structures or laminates made from epoxy resin impregnated carbon "fibrous or filamentary materials" for the repair of "civil aircraft" structures or laminates, having all of the following:a.An area not exceeding 1 m2;b.A length not exceeding 2,5 m; andc.A width exceeding 15 mm.Note 2:1A002 does not control semi-finished items, specially designed for purely civilian applications as follows:a.Sporting goods;b.Automotive industry;c.Machine tool industry;d.Medical applications.Note 3:1A002.b.1. does not control semi-finished items containing a maximum of two dimensions of interwoven filaments and specially designed for applications as follows:a.Metal heat-treatment furnaces for tempering metals;b.Silicon boule production equipment.Note 4:1A002 does not control finished items specially designed for a specific application.	M6A1	Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A.
1A102	Resaturated pyrolized carbon-carbon components designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.	M6A2	Resaturated pyrolised (i.e. carbon-carbon) components having all of the following: a. Designed for rocket systems; and b. Usable in the systems specified in 1.A. or 19.A.1.

1BTest, Inspection and Production Equipment

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
1B001	Equipment for the production or inspection of "composite" structures or laminates specified in 1A002 or "fibrous or filamentary materials" specified in 1C010, as follows, and specially designed components and accessories therefor:N.B.:SEE ALSO 1B101 AND 1B201.
	a.Filament winding machines, of which the motions for positioning, wrapping and winding fibres are coordinated and programmed in three or more "primary servo positioning" axes, specially designed for the manufacture of "composite" structures or laminates, from "fibrous or filamentary materials";	M6B1a	Filament winding machines or "fibre/tow-placement machines", of which the motions for positioning, wrapping and winding fibres can be coordinated and programmed in three or more axes, designed to fabricate composite structures or laminates from fibrous or filamentary materials, and co-ordinating and programming controls
	b."Tape-laying machines", of which the motions for positioning and laying tape are coordinated and programmed in five or more "primary servo positioning" axes, specially designed for the manufacture of "composite" airframe or "missile" structures;Note:In 1B001.b., "missile" means complete rocket systems and unmanned aerial vehicle systems.Technical Note:For the purposes of 1B001.b., "tape-laying machines" have the ability to lay one or more "filament bands" limited to widths greater than 25 mm and less than or equal to 305 mm, and to cut and restart individual "filament band" courses during the laying process.	M6B1b	"Tape-laying machines" of which the motions for positioning and laying tape can be co-ordinated and programmed in two or more axes, designed for the manufacture of composite airframes and missile structures;Note:For the purposes of 6.B.1.a. and 6.B.1.b., the following definitions apply:1.A "filament band" is a single continuous width of fully or partially resinimpregnated tape, tow, or fibre. Fully or partially resin-impregnated "filament bands" include those coated with dry powder that tacks upon heating.2."Fibre/tow-placement machines" and "tape-laying machines" are machines that perform similar processes that use computer-guided heads to lay one or several "filament bands" onto a mold to create a part or a structure. These machines have the ability to cut and restart individual "filament band" courses during the laying process.3."Fibre/tow-placement machines" have the ability to place one or more "filament bands" having widths less than or equal to 25,4 mm. This refers to the minimum width of material the machine can place, regardless of the upper capability of the machine.4."Tape-laying machines" have the ability to place one or more "filament bands" having widths less than or equal to 304,8 mm, but cannot place "filaments bands" with a width equal to or less than 25,4 mm. This refers to the minimum width of material the machine can place, regardless of the upper capability of the machine.
	c.Multidirectional, multidimensional weaving machines or interlacing machines, including adapters and modification kits, specially designed or modified for weaving, interlacing or braiding fibres, for "composite" structures;Technical Note:For the purposes of 1B001.c., the technique of interlacing includes knitting.	M6B1c	Multi-directional, multi-dimensional weaving machines or interlacing machines, including adapters and modification kits for weaving, interlacing or braiding fibres to manufacture composite structures;Note:6.B.1.c. does not control textile machinery not modified for the end-uses stated.
	d.Equipment specially designed or adapted for the production of reinforcement fibres, as follows:		Equipment designed or modified for the production of fibrous or filamentary materials as follows:
	1.Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon, pitch or polycarbosilane) into carbon fibres or silicon carbide fibres, including special equipment to strain the fibre during heating;	M6B1d1	1.Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon, or polycarbosilane) including special provision to strain the fibre during heating;
	2.Equipment for the chemical vapour deposition of elements or compounds, on heated filamentary substrates, to manufacture silicon carbide fibres;	M6B1d2	2.Equipment for the vapour deposition of elements or compounds on heated filament substrates;
	3.Equipment for the wet-spinning of refractory ceramics (such as aluminium oxide);	M6B1d3	3.Equipment for the wet-spinning of refractory ceramics (such as aluminium oxide)
	4.Equipment for converting aluminium containing precursor fibres into alumina fibres by heat treatment;e.Equipment for producing prepregs specified in 1C010.e. by the hot melt method;f.Non-destructive inspection equipment specially designed for "composite" materials, as follows:1.X-ray tomography systems for three dimensional defect inspection;2.Numerically controlled ultrasonic testing machines of which the motions for positioning transmitters or receivers are simultaneously coordinated and programmed in four or more axes to follow the three dimensional contours of the component under inspection;g."Tow-placement machines", of which the motions for positioning and laying tows are coordinated and programmed in two or more "primary servo positioning" axes, specially designed for the manufacture of "composite" airframe or "missile" structures.Technical Note:For the purposes of 1B001.g., "tow-placement machines" have the ability to place one or more "filament bands" having widths less than or equal to 25 mm, and to cut and restart individual "filament band" courses during the placement process.Technical Note:1.For the purpose of 1B001, "primary servo positioning" axes control, under computer program direction, the position of the end effector (i.e., head) in space relative to the work piece at the correct orientation and direction to achieve the desired process.2.For the purposes of 1B001., a "filament band" is a single continuous width of fully or partially resin-impregnated tape, tow or fibre.	M6B1e	Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms, including rollers, tension stretchers, coating equipment, cutting equipment and clicker dies.Note:Examples of components and accessories for the machines specified in 6.B.1. are moulds, mandrels, dies, fixtures and tooling for the preform pressing, curing, casting, sintering or bonding of composite structures, laminates and manufactures thereof
1B002	Equipment for producing metal alloys, metal alloy powder or alloyed materials, specially designed to avoid contamination and specially designed for use in one of the processes specified in 1C002.c.2.N.B.:SEE ALSO 1B102.	M4B3d	Metal powder "production equipment" usable for the "production", in a controlled environment, of spherical, spheroidal or atomised materials specified in 4.C.2.c., 4.C.2.d. or 4.C.2.e. Note: 4.B.3.d. includes: a. Plasma generators (high frequency arc-jet) usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment; b. Electroburst equipment usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment; c. Equipment usable for the "production" of spherical aluminium powders by powdering a melt in an inert medium (e.g. nitrogen).Notes:1.The only batch mixers, continuous mixers, usable for solid propellants or propellants constituents specified in 4.C., and fluid energy mills specified in 4.B., are those specified in 4.B.3.2.Forms of metal powder "production equipment" not specified in 4.B.3.d. are to be evaluated in accordance with 4.B.2.
1B101	Equipment, other than that specified in 1B001, for the "production" of structural composites as follows; and specially designed components and accessories therefor:N.B.:SEE ALSO 1B201.Note:Components and accessories specified in 1B101 include moulds, mandrels, dies, fixtures and tooling for the preform pressing, curing, casting, sintering or bonding of composite structures, laminates and manufactures thereof.
	a.Filament winding machines or fibre placement machines, of which the motions for positioning, wrapping and winding fibres can be coordinated and programmed in three or more axes, designed to fabricate composite structures or laminates from fibrous or filamentary materials, and coordinating and programming controls;	M6B1a	Filament winding machines or "fibre/tow-placement machines", of which the motions for positioning, wrapping and winding fibres can be coordinated and programmed in three or more axes, designed to fabricate composite structures or laminates from fibrous or filamentary materials, and co-ordinating and programming controls;
	b.Tape-laying machines of which the motions for positioning and laying tape and sheets can be coordinated and programmed in two or more axes, designed for the manufacture of composite airframe and "missile" structures;	M6B1b	"Tape-laying machines" of which the motions for positioning and laying tape can be co-ordinated and programmed in two or more axes, designed for the manufacture of composite airframes and missile structures;Note:For the purposes of 6.B.1.a. and 6.B.1.b., the following definitions apply:1.A "filament band" is a single continuous width of fully or partially resinimpregnated tape, tow, or fibre. Fully or partially resin-impregnated "filament bands" include those coated with dry powder that tacks upon heating.2."Fibre/tow-placement machines" and "tape-laying machines" are machines that perform similar processes that use computer-guided heads to lay one or several "filament bands" onto a mold to create a part or a structure. These machines have the ability to cut and restart individual "filament band" courses during the laying process.3."Fibre/tow-placement machines" have the ability to place one or more "filament bands" having widths less than or equal to 25,4 mm. This refers to the minimum width of material the machine can place, regardless of the upper capability of the machine.4."Tape-laying machines" have the ability to place one or more "filament bands" having widths less than or equal to 304,8 mm, but cannot place "filaments bands" with a width equal to or less than 25,4 mm. This refers to the minimum width of material the machine can place, regardless of the upper capability of the machine.
	c.Equipment designed or modified for the "production" of "fibrous or filamentary materials" as follows:1.Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon or polycarbosilane) including special provision to strain the fibre during heating;2.Equipment for the vapour deposition of elements or compounds on heated filament substrates;3.Equipment for the wet-spinning of refractory ceramics (such as aluminium oxide);	M6B1d	Equipment designed or modified for the production of fibrous or filamentary materials as follows:1.Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon, or polycarbosilane) including special provision to strain the fibre during heating;2.Equipment for the vapour deposition of elements or compounds on heated filament substrates;3.Equipment for the wet-spinning of refractory ceramics (such as aluminium oxide);
	d.Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms specified in entry 9C110.Note:1B101.d. includes rollers, tension stretchers, coating equipment, cutting equipment and clicker dies.	M6B1e	Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms, including rollers, tension stretchers, coating equipment, cutting equipment and clicker dies.Note:Examples of components and accessories for the machines specified in 6.B.1. are moulds, mandrels, dies, fixtures and tooling for the preform pressing, curing, casting, sintering or bonding of composite structures, laminates and manufactures thereof
1B102	Metal powder "production equipment", other than that specified in 1B002, and components as follows:N.B.:SEE ALSO 1B115.b.a.Metal powder "production equipment" usable for the "production", in a controlled environment, of spherical, spheroidal or atomised materials specified in 1C011.a., 1C011.b., 1C111.a.1., 1C111.a.2. or in the Military Goods Controls.b.Specially designed components for "production equipment" specified in 1B002 or 1B102.a.Note:1B102 includes:a.Plasma generators (high frequency arc-jet) usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment;b.Electroburst equipment usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment;c.Equipment usable for the "production" of spherical aluminium powders by powdering a melt in an inert medium (e.g. nitrogen).	M4B3d	Metal powder "production equipment" usable for the "production", in a controlled environment, of spherical, spheroidal or atomised materials specified in 4.C.2.c., 4.C.2.d. or 4.C.2.e.Note:4.B.3.d. includes:a.Plasma generators (high frequency arc-jet) usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment;b.Electroburst equipment usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment;c.Equipment usable for the "production" of spherical aluminium powders by powdering a melt in an inert medium (e.g. nitrogen).Notes:1.The only batch mixers, continuous mixers, usable for solid propellants or propellants constituents specified in 4.C., and fluid energy mills specified in 4.B., are those specified in 4.B.3.2.Forms of metal powder "production equipment" not specified in 4.B.3.d. are to be evaluated in accordance with 4.B.2.
1B115	Equipment, other than that specified in 1B002 or 1B102, for the production of propellant and propellant constituents, as follows, and specially designed components therefor:
	a."Production equipment" for the "production", handling or acceptance testing of liquid propellants or propellant constituents specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls;	M4B1	"Production equipment", and specially designed components therefor, for the "production", handling or acceptance testing of liquid propellants or propellant constituents specified in 4.C.
	b."Production equipment" for the "production", handling, mixing, curing, casting, pressing, machining, extruding or acceptance testing of solid propellants or propellant constituents specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls.Note:1B115.b. does not control batch mixers, continuous mixers or fluid energy mills. For the control of batch mixers, continuous mixers and fluid energy mills see 1B117, 1B118 and 1B119.Note 1:For equipment specially designed for the production of military goods, see the Military Goods Controls.Note 2:1B115 does not control equipment for the "production", handling and acceptance testing of boron carbide.	M4B2	"Production equipment", other than that described in 4.B.3., and specially designed components therefor, for the production, handling, mixing, curing, casting, pressing, machining, extruding or acceptance testing of solid propellants or propellant constituents specified in 4.C.
1B116	Specially designed nozzles for producing pyrolitically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1573 K (1300 °C) to 3173 K (2900 °C) temperature range at pressures of 130 Pa to 20 kPa.	M6B2	Nozzles specially designed for the processes referred to in 6.E.3.
1B117	Batch mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with temperature control capability of the mixing chamber and having all of the following, and specially designed components therefor:a.A total volumetric capacity of 110 litres or more; andb.At least one "mixing/kneading shaft" mounted off centre.Note:In 1B117.b. the term "mixing/kneading shaft" does not refer to deagglomerators or knife-spindles.	M4B3a	Batch mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with temperature control capability of the mixing chamber and having all of the following:1.A total volumetric capacity of 110 litres or more; and2.At least one "mixing/kneading shaft" mounted off centre;Note:In Item 4.B.3.a.2. the term "mixing/kneading shaft" does not refer to deagglomerators or knife-spindles.
1B118	Continuous mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with a temperature control capability of the mixing chamber having any of the following, and specially designed components therefor:a.Two or more mixing/kneading shafts; orb.A single rotating shaft which oscillates and having kneading teeth/pins on the shaft as well as inside the casing of the mixing chamber.	M4B3b	Continuous mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with a temperature control capability of the mixing chamber having any of the following:1.Two or more mixing/kneading shafts; or2.A single rotating shaft which oscillates and having kneading teeth/pins on the shaft as well as inside the casing of the mixing chamber;
1B119	Fluid energy mills usable for grinding or milling substances specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls, and specially designed components therefor.	M4B3c	Fluid energy mills usable for grinding or milling substances specified in 4.C

1CMaterials

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
1C001	Materials specially designed for use as absorbers of electromagnetic waves, or intrinsically conductive polymers, as follows:N.B.:SEE ALSO 1C101.a.Materials for absorbing frequencies exceeding 2 × 108 Hz but less than 3 × 1012 Hz;Note 1:1C001.a. does not control:a.Hair type absorbers, constructed of natural or synthetic fibres, with non-magnetic loading to provide absorption;b.Absorbers having no magnetic loss and whose incident surface is non-planar in shape, including pyramids, cones, wedges and convoluted surfaces;c.Planar absorbers, having all of the following:1.Made from any of the following:a.Plastic foam materials (flexible or non-flexible) with carbon-loading, or organic materials, including binders, providing more than 5 % echo compared with metal over a bandwidth exceeding ± 15 % of the centre frequency of the incident energy, and not capable of withstanding temperatures exceeding 450 K (177 °C); orb.Ceramic materials providing more than 20 % echo compared with metal over a bandwidth exceeding ± 15 % of the centre frequency of the incident energy, and not capable of withstanding temperatures exceeding 800 K (527 °C);Technical Note:Absorption test samples for 1C001.a. Note: 1.c.1. should be a square at least 5 wavelengths of the centre frequency on a side and positioned in the far field of the radiating element.2.Tensile strength less than 7 × 106 N/m2; and3.Compressive strength less than 14 × 106 N/m2;d.Planar absorbers made of sintered ferrite, having all of the following:1.A specific gravity exceeding 4,4; and2.A maximum operating temperature of 548 K (275 °C).Note 2:Nothing in Note 1 to 1C001.a. releases magnetic materials to provide absorption when contained in paint.b.Materials for absorbing frequencies exceeding 1,5 × 1014 Hz but less than 3,7 × 1014 Hz and not transparent to visible light;Note:1C001.b. does not control materials, specially designed or formulated for any of the following applications:a.Laser marking of polymers; orb.Laser welding of polymers.c.Intrinsically conductive polymeric materials with a "bulk electrical conductivity" exceeding 10000 S/m (Siemens per metre) or a "sheet (surface) resistivity" of less than 100 ohms/square, based on any of the following polymers:1.Polyaniline;2.Polypyrrole;3.Polythiophene;4.Poly phenylene-vinylene; or5.Poly thienylene-vinylene.Note:1C001.c. does not control materials in a liquid form.Technical Note:"Bulk electrical conductivity" and "sheet (surface) resistivity" should be determined using ASTM D-257 or national equivalents.	M17C1	Materials for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures (i.e. stealth technology), for applications usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A.Notes:1.17.C.1. includes structural materials and coatings (including paints), specially designed for reduced or tailored reflectivity or emissivity in the microwave, infrared or ultraviolet spectra.2.17.C.1. does not control coatings (including paints) when specially used for thermal control of satellites.
1C007	Ceramic powders, non-"composite" ceramic materials, ceramic-"matrix" "composite" materials and precursor materials, as follows:N.B.:SEE ALSO 1C107.	M6C5	Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in missile radomes usable in systems specified in 1.A. or 19.A.1.
	a.Ceramic powders of single or complex borides of titanium, having total metallic impurities, excluding intentional additions, of less than 5000 ppm, an average particle size equal to or less than 5 μm and no more than 10 % of the particles larger than 10 μm;b.Non-"composite" ceramic materials in crude or semi-fabricated form, composed of borides of titanium with a density of 98 % or more of the theoretical density;Note:1C007.b. does not control abrasives.c.Ceramic-ceramic "composite" materials with a glass or oxide-"matrix" and reinforced with fibres having all of the following:1.Made from any of the following materials:a.Si-N;b.Si-C;c.Si-Al-O-N; ord.Si-O-N; and2.Having a "specific tensile strength" exceeding 12,7 × 103m;d.Ceramic-ceramic "composite" materials, with or without a continuous metallic phase, incorporating particles, whiskers or fibres, where carbides or nitrides of silicon, zirconium or boron form the "matrix";e.Precursor materials (i.e., special purpose polymeric or metallo-organic materials) for producing any phase or phases of the materials specified in 1C007.c., as follows:1.Polydiorganosilanes (for producing silicon carbide);2.Polysilazanes (for producing silicon nitride);3.Polycarbosilazanes (for producing ceramics with silicon, carbon and nitrogen components);f.Ceramic-ceramic "composite" materials with an oxide or glass "matrix" reinforced with continuous fibres from any of the following systems:1.Al2O3 (CAS 1344-28-1); or2.Si-C-N.Note:1C007.f. does not control "composites" containing fibres from these systems with a fibre tensile strength of less than 700 MPa at 1273 K (1000 °C) or fibre tensile creep resistance of more than 1 % creep strain at 100 MPa load and 1273 K (1000 °C) for 100 hours.	M6C6	Silicon-carbide materials as follows:a.Bulk machinable silicon-carbide reinforced unfired ceramic usable for nose tips usable in systems specified in 1.A. or 19.A.1.;Reinforced silicon-carbide ceramic composites usable for nose tips, re-entry vehicles, nozzle flaps, usable in systems specified in 1.A. or 19.A.1.
1C010	"Fibrous or filamentary materials", as follows:N.B.:SEE ALSO 1C210 AND 9C110.a.Organic "fibrous or filamentary materials", having all of the following:1."Specific modulus" exceeding 12,7 × 106 m; and2."Specific tensile strength" exceeding 23,5 × 104 m;Note:1C010.a. does not control polyethylene.b.Carbon "fibrous or filamentary materials", having all of the following:1."Specific modulus" exceeding 14,65 × 106 m; and2."Specific tensile strength" exceeding 26,82 × 104 m;Note:1C010.b. does not control:a."Fibrous or filamentary materials", for the repair of "civil aircraft" structures or laminates, having all of the following:1.An area not exceeding 1 m2;2.A length not exceeding 2,5 m; and3.A width exceeding 15 mm.b.Mechanically chopped, milled or cut carbon "fibrous or filamentary materials" 25,0 mm or less in length.c.Inorganic "fibrous or filamentary materials", having all of the following:1."Specific modulus" exceeding 2,54 × 106 m; and2.Melting, softening, decomposition or sublimation point exceeding 1922 K (1649 °C) in an inert environment;Note:1C010.c. does not control:a.Discontinuous, multiphase, polycrystalline alumina fibres in chopped fibre or random mat form, containing 3 % by weight or more silica, with a "specific modulus" of less than 10 × 106 m;b.Molybdenum and molybdenum alloy fibres;c.Boron fibres;d.Discontinuous ceramic fibres with a melting, softening, decomposition or sublimation point lower than 2043 K (1770 °C) in an inert environment.Technical Notes:1.For the purpose of calculating "specific tensile strength", "specific modulus" or specific weight of "fibrous or filamentary materials" in 1C010.a., 1C010.b. or 1C010.c., the tensile strength and modulus should be determined by using Method A described in ISO 10618 (2004) or national equivalents.2.Assessing the "specific tensile strength", "specific modulus" or specific weight of non-unidirectional "fibrous or filamentary materials" (e.g., fabrics, random mats or braids) in 1C010. is to be based on the mechanical properties of the constituent unidirectional monofilaments (e.g., monofilaments, yarns, rovings or tows) prior to processing into the non-unidirectional "fibrous or filamentary materials".d."Fibrous or filamentary materials", having any of the following:1.Composed of any of the following:a.Polyetherimides specified in 1C008.a.; orb.Materials specified in 1C008.b. to 1C008.f.; or2.Composed of materials specified in 1C010.d.1.a. or 1C010.d.1.b. and "commingled" with other fibres specified in 1C010.a., 1C010.b. or 1C010.c.;
	e.Fully or partially resin-impregnated or pitch-impregnated "fibrous or filamentary materials" (prepregs), metal or carbon-coated "fibrous or filamentary materials" (preforms) or "carbon fibre preforms", having all of the following:1.Having any of the following:a.Inorganic "fibrous or filamentary materials" specified in 1C010.c.; orb.Organic or carbon "fibrous or filamentary materials", having all of the following:1."Specific modulus" exceeding 10,15 × 106 m; and2."Specific tensile strength" exceeding 17,7 × 104 m; and2.Having any of the following:a.Resin or pitch, specified in 1C008 or 1C009.b.;b."Dynamic Mechanical Analysis glass transition temperature (DMA Tg)" equal to or exceeding 453 K (180 °C) and having a phenolic resin; orc."Dynamic Mechanical Analysis glass transition temperature (DMA Tg)" equal to or exceeding 505 K (232 °C) and having a resin or pitch, not specified in 1C008 or 1C009.b., and not being a phenolic resin;Note 1:Metal or carbon-coated "fibrous or filamentary materials" (preforms) or "carbon fibre preforms", not impregnated with resin or pitch, are specified by "fibrous or filamentary materials" in 1C010.a., 1C010.b. or 1C010.c.Note 2:1C010.e. does not control:a.Epoxy resin "matrix" impregnated carbon "fibrous or filamentary materials" (prepregs) for the repair of "civil aircraft" structures or laminates, having all the following;1.An area not exceeding 1 m2;2.A length not exceeding 2,5 m; and3.A width exceeding 15 mm.b.Fully or partially resin-impregnated or pitch-impregnated mechanically chopped, milled or cut carbon "fibrous or filamentary materials" 25,0 mm or less in length when using a resin or pitch other than those specified by 1C008 or 1C009.b.Technical Note:The "Dynamic Mechanical Analysis glass transition temperature (DMA Tg)" for materials specified by 1C010.e. is determined using the method described in ASTM D 7028-07, or equivalent national standard, on a dry test specimen. In the case of thermoset materials, degree of cure of a dry test specimen shall be a minimum of 90 % as defined by ASTM E 2160-04 or equivalent national standard.	M6C1	Resin impregnated fibre prepregs and metal coated fibre preforms, for the goods specified in 6.A.1., made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a specific tensile strength greater than 7,62 × 104 m and a specific modulus greater than 3,18 × 106 m.Note:The only resin impregnated fibre prepregs specified in 6.C.1. are those using resins with a glass transition temperature (Tg), after cure, exceeding 145 °C as determined by ASTM D4065 or national equivalents.Technical Notes:1.In Item 6.C.1. "specific tensile strength" is the ultimate tensile strength in N/m2 divided by the specific weight in N/m3, measured at a temperature of (296 ± 2)K ((23 ± 2)°C) and a relative humidity of (50 ± 5)%.2.In Item 6.C.1. "specific modulus" is the Young's modulus in N/m2 divided by the specific weight in N/m3, measured at a temperature of (296 ± 2)K ((23 ± 2)°C) and a relative humidity of (50 ± 5)%.
1C011	Metals and compounds, as follows:N.B.:SEE ALSO 1C111.
	a.Metals in particle sizes of less than 60 μm whether spherical, atomised, spheroidal, flaked or ground, manufactured from material consisting of 99 % or more of zirconium, magnesium and alloys thereof;Technical Note:The natural content of hafnium in the zirconium (typically 2 % to 7 %) is counted with the zirconium.Note:The metals or alloys specified in 1C011.a. are controlled whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium.	M4C2d	Metal powders of any of the following: zirconium (CAS 7440-67-7), beryllium (CAS 7440-41-7), magnesium (CAS 7439-95-4) or alloys of these, if at least 90 % of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spheroidal, flaked or ground, consisting of 97 % by weight or more of any of the above mentioned metals;Note:In a multimodal particle distribution (e.g. mixtures of different grain sizes) in which one or more modes are controlled, the entire powder mixture is controlled.Technical Note:The natural content of hafnium (CAS 7440-58-6) in the zirconium (typically 2 % to 7 %) is counted with the zirconium.
	b.Boron or boron alloys, with a particle size of 60 μm or less, as follows:1.Boron with a purity of 85 % by weight or more;2.Boron alloys with a boron content of 85 % by weight or more;Note:The metals or alloys specified in 1C011.b. are controlled whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium.c.Guanidine nitrate (CAS 506-93-4);d.Nitroguanidine (NQ) (CAS 556-88-7).N.B.:See also Military Goods Controls for metal powders mixed with other substances to form a mixture formulated for military purposes.	M4C2e	Metal powders of either boron (CAS 7440-42-8) or boron alloys with a boron content of 85 % or more by weight, if at least 90 % of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spheroidal, flaked or ground;Note:In a multimodal particle distribution (e.g. mixtures of different grain sizes) in which one or more modes are controlled, the entire powder mixture is controlled.
1C101	Materials and devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures, other than those specified in 1C001, usable in "missiles", "missile" subsystems or unmanned aerial vehicles specified in 9A012 or 9A112.a.Note 1:1C101 includes:a.Structural materials and coatings specially designed for reduced radar reflectivity;b.Coatings, including paints, specially designed for reduced or tailored reflectivity or emissivity in the microwave, infrared or ultraviolet regions of the electromagnetic spectrum.Note 2:1C101 does not include coatings when specially used for the thermal control of satellites.Technical Note:In 1C101 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M17A1	Devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures (i.e. stealth technology), for applications usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A. or 20.A.
		M17C1	Materials for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures (i.e. stealth technology), for applications usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A.Notes:1.17.C.1. includes structural materials and coatings (including paints), specially designed for reduced or tailored reflectivity or emissivity in the microwave, infrared or ultraviolet spectra.2.17.C.1. does not control coatings (including paints) when specially used for thermal control of satellites.
1C102	Resaturated pyrolized carbon-carbon materials designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.	M6C2	Resaturated pyrolised (i.e. carbon-carbon) materials having all of the following: a. Designed for rocket systems; and b. Usable in the systems specified in 1.A. or 19.A.1.
1C107	Graphite and ceramic materials, other than those specified in 1C007, as follows:
	a.Fine grain graphites with a bulk density of 1,72 g/cm3 or greater, measured at 288 K (15 °C), and having a grain size of 100 μm or less, usable for rocket nozzles and re-entry vehicle nose tips, which can be machined to any of the following products:1.Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater;2.Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; or3.Blocks having a size of 120 mm × 120 mm × 50 mm or greater;N.B.:See also 0C004	M6C3	Fine grain graphites with a bulk density of at least 1,72 g/cc measured at 15 °C and having a grain size of 100 × 10-6 m (100 μm) or less, usable for rocket nozzles and re-entry vehicle nose tips, which can be machined to any of the following products:a.Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater;b.Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; orc.Blocks having a size of 120 mm × 120 mm × 50 mm or greater
	b.Pyrolytic or fibrous reinforced graphites, usable for rocket nozzles and reentry vehicle nose tips usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;N.B.:See also 0C004	M6C4	Pyrolytic or fibrous reinforced graphites usable for rocket nozzles and reentry vehicle nose tips usable in systems specified in 1.A. or 19.A.1.
	c.Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in radomes usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;	M6C5	Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in missile radomes usable in systems specified in 1.A. or 19.A.1.
	d.Bulk machinable silicon-carbide reinforced unfired ceramic, usable for nose tips usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;	M6C6a	Bulk machinable silicon-carbide reinforced unfired ceramic usable for nose tips usable in systems specified in 1.A. or 19.A.1.;
	e.Reinforced silicon-carbide ceramic composites, usable for nose tips, reentry vehicles and nozzle flaps usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.	M6C6b	Reinforced silicon-carbide ceramic composites usable for nose tips, re-entry vehicles, nozzle flaps, usable in systems specified in 1.A. or 19.A.1.
1C111	Propellants and constituent chemicals for propellants, other than those specified in 1C011, as follows:a.Propulsive substances:
	1.Spherical or spheroidal aluminium powder other than that specified in the Military Goods Controls, in particle size of less than 200 μm and an aluminium content of 97 % by weight or more, if at least 10 % of the total weight is made up of particles of less than 63 μm, according to ISO 2591-1:1988 or national equivalents;Technical Note:A particle size of 63 μm (ISO R-565) corresponds to 250 mesh (Tyler) or 230 mesh (ASTM standard E-11).2.Metal powders, other than that specified in the Military Goods Controls, as follows:	M4C2c	Spherical or spheroidal aluminium powder (CAS 7429-90-5) in particle size of less than 200 × 10-6 m (200 μm) and an aluminium content of 97 % by weight or more, if at least 10 % of the total weight is made up of particles of less than 63 μm, according to ISO 2591-1:1988 or national equivalents;Technical Note:A particle size of 63 μm (ISO R-565) corresponds to 250 mesh (Tyler) or 230 mesh (ASTM standard E-11).
	a.Metal powders of zirconium, beryllium or magnesium, or alloys of these metals, if at least 90 % of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomized, spheroidal, flaked or ground, consisting 97 % by weight or more of any of the following:1.Zirconium;2.Beryllium; or3.Magnesium;Technical Note:The natural content of hafnium in the zirconium (typically 2 % to 7 %) is counted with the zirconium.	M4C2d	Metal powders of any of the following: zirconium (CAS 7440-67-7), beryllium (CAS 7440-41-7), magnesium (CAS 7439-95-4) or alloys of these, if at least 90 % of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spheroidal, flaked or ground, consisting of 97 % by weight or more of any of the above mentioned metals;Note:In a multimodal particle distribution (e.g. mixtures of different grain sizes) in which one or more modes are controlled, the entire powder mixture is controlled.Technical Note:The natural content of hafnium (CAS 7440-58-6) in the zirconium (typically 2 % to 7 %) is counted with the zirconium.
	b.Metal powders of either boron or boron alloys with a boron content of 85 % or more by weight, if at least 90 % of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spheroidal, flaked or ground;Note:1C111a.2.a. and 1C111a.2.b. controls powder mixtures with a multimodal particle distribution (e.g. mixtures of different grain sizes) if one or more modes are controlled.	M4C2e	Metal powders of either boron (CAS 7440-42-8) or boron alloys with a boron content of 85 % or more by weight, if at least 90 % of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spheroidal, flaked or groundNote:In a multimodal particle distribution (e.g. mixtures of different grain sizes) in which one or more modes are controlled, the entire powder mixture is controlled.
	3.Oxidiser substances usable in liquid propellant rocket engines as follows:a.Dinitrogen trioxide (CAS 10544-73-7);b.Nitrogen dioxide (CAS 10102-44-0)/dinitrogen tetroxide (CAS 10544-72-6);c.Dinitrogen pentoxide (CAS 10102-03-1);d.Mixed Oxides of Nitrogen (MON);Technical Note:Mixed Oxides of Nitrogen (MON) are solutions of Nitric Oxide (NO) in Dinitrogen Tetroxide/Nitrogen Dioxide (N2O4/NO2 ) that can be used in missile systems. There are a range of compositions that can be denoted as MONi or MONij, where i and j are integers representing the percentage of Nitric Oxide in the mixture (e.g., MON3 contains 3 % Nitric Oxide, MON25 25 % Nitric Oxide. An upper limit is MON40, 40 % by weight).e.SEE MILITARY GOODS CONTROLS FOR Inhibited Red Fuming Nitric Acid (IRFNA);f.SEE MILITARY GOODS CONTROLS AND 1C238 FOR Compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen;	M4C4a	Oxidiser substances usable in liquid propellant rocket engines as follows:1.Dinitrogen trioxide (CAS 10544-73-7)2.Nitrogen dioxide (CAS 10102-44-0) / dinitrogen tetroxide (CAS 10544-72-6);3.Dinitrogen pentoxide (CAS 10102-03-1);4.Mixed Oxides of Nitrogen (MON);Technical Note:Mixed Oxides of Nitrogen (MON) are solutions of Nitric Oxide (NO) in Dinitrogen Tetroxide/Nitrogen Dioxide (N2O4/NO2) that can be used in missile systems. There are a range of compositions that can be denoted as MONi or MONij where i and j are integers representing the percentage of Nitric Oxide in the mixture (e.g. MON3 contains 3 % Nitric Oxide, MON25 25 % Nitric Oxide. An upper limit is MON40, 40 % by weight).5.Inhibited Red Fuming Nitric Acid (IRFNA) (CAS 8007-58-7);6.Compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen;Note:Item 4.C.4.a.6. does not control Nitrogen Trifluoride (NF3) (CAS 7783-54- 2) in a gaseous state as it is not usable for missile applications.
	4.Hydrazine derivatives as follows:N.B.:SEE ALSO MILITARY GOODS CONTROLS.a.Trimethylhydrazine (CAS 1741-01-1);b.Tetramethylhydrazine (CAS 6415-12-9);c.N,N diallylhydrazine (CAS 5164-11-4);d.Allylhydrazine (CAS 7422-78-8);e.Ethylene dihydrazine;f.Monomethylhydrazine dinitrate;g.Unsymmetrical dimethylhydrazine nitrate;h.Hydrazinium azide (CAS 14546-44-2);i.Dimethylhydrazinium azide;j.Hydrazinium dinitrate (CAS 13464-98-7);k.Diimido oxalic acid dihydrazine (CAS 3457-37-2);l.2-hydroxyethylhydrazine nitrate (HEHN);m.See Military Goods Controls for Hydrazinium perchlorate;n.Hydrazinium diperchlorate (CAS 13812-39-0);o.Methylhydrazine nitrate (MHN) (CAS 29674-96-2);p.Diethylhydrazine nitrate (DEHN);q.3,6-dihydrazino tetrazine nitrate (1,4-dihydrazine nitrate) (DHTN);	M4C2b	Hydrazine derivatives as follows:1.Monomethylhydrazine (MMH) (CAS 60-34-4);2.Unsymmetrical dimethylhydrazine (UDMH) (CAS 57-14-7);3.Hydrazine mononitrate (CAS 13464-97-6);4.Trimethylhydrazine (CAS 1741-01-1);5.Tetramethylhydrazine (CAS 6415-12-9);6.N,N diallylhydrazine (CAS 5164-11-4);7.Allylhydrazine (CAS 7422-78-8);8.Ethylene dihydrazine (CAS 6068-98-0);9.Monomethylhydrazine dinitrate;10.Unsymmetrical dimethylhydrazine nitrate;11.Hydrazinium azide (CAS 14546-44-2);12.1,1-Dimethylhydrazinium azide (CAS 227955-52-4) / 1,2-Dimethylhydrazinium azide (CAS 299177-50-7);13.Hydrazinium dinitrate (CAS 13464-98-7);14.Diimido oxalic acid dihydrazine (CAS 3457-37-2);15.2-hydroxyethylhydrazine nitrate (HEHN);16.Hydrazinium perchlorate (CAS 27978-54-7);17.Hydrazinium diperchlorate (CAS 13812-39-0);18.Methylhydrazine nitrate (MHN) (CAS 29674-96-2);19.1,1-Diethylhydrazine nitrate (DEHN) / 1,2-Diethylhydrazine nitrate (DEHN) (CAS 363453-17-2);20.3,6-dihydrazino tetrazine nitrate (DHTN);Technical note:3,6-dihydrazino tetrazine nitrate is also referred to as 1,4-dihydrazine nitrate.
	5.High energy density materials, other than that specified in the Military Goods Controls, usable in "missiles" or unmanned aerial vehicles specified in 9A012 or 9A112.a.;a.Mixed fuel that incorporate both solid and liquid fuels, such as boron slurry, having a mass-based energy density of 40 × 106 J/kg or greater;b.Other high energy density fuels and fuel additives (e.g., cubane, ionic solutions, JP-10) having a volume-based energy density of 37,5 × 109 J/m3 or greater, measured at 20 °C and one atmosphere (101,325 kPa) pressure;Note:1C111.a.5.b. does not control fossil refined fuels and biofuels produced from vegetables, including fuels for engines certified for use in civil aviation, unless specially formulated for "missiles" or unmanned aerial vehicles specified in 9A012 or 9A112.a..Technical Note:In 1C111.a.5. "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M4C2f	High energy density materials, usable in the systems specified in 1.A. or 19.A., as follows:1.Mixed fuels that incorporate both solid and liquid fuels, such as boron slurry, having a mass- based energy density of 40 × 106 J/kg or greater;2.Other high energy density fuels and fuel additives (e.g., cubane, ionic solutions, JP-10) having a volume-based energy density of 37,5 × 109 J/m3 or greater, measured at 20 °C and one atmosphere (101,325 kPa) pressure.Note:Item 4.C.2.f.2. does not control fossil refined fuels and biofuels produced from vegetables, including fuels for engines certified for use in civil aviation, unless specifically formulated for systems specified in 1.A. or 19.A.
	6.Hydrazine replacement fuels as follows:a.2-Dimethylaminoethylazide (DMAZ) (CAS 86147-04-8);	M4C2g	Hydrazine replacement fuels as follows: 1. 2-Dimethylaminoethylazide (DMAZ) (CAS 86147-04-8).
	b.Polymeric substances:1.Carboxy-terminated polybutadiene (including carboxyl-terminated polybutadiene) (CTPB);2.Hydroxy-terminated polybutadiene (including hydroxyl-terminated polybutadiene) (HTPB), other than that specified in the Military Goods Controls;3.Polybutadiene-acrylic acid (PBAA);4.Polybutadiene-acrylic acid-acrylonitrile (PBAN);5.Polytetrahydrofuran polyethylene glycol (TPEG);Technical Note:Polytetrahydrofuran polyethylene glycol (TPEG) is a block co-polymer of poly 1,4-Butanediol (CAS 110-63-4) and polyethylene glycol (PEG) (CAS 25322-68-3).6.Polyglycidyl nitrate (PGN or poly-GLYN) (CAS 27814-48-8).	M4C5	Polymeric substances, as follows:a.Carboxy — terminated polybutadiene (including carboxyl — terminated polybutadiene) (CTPB);b.Hydroxy — terminated polybutadiene (including hydroxyl — terminated polybutadiene) (HTPB);c.Glycidyl azide polymer (GAP);d.Polybutadiene — Acrylic Acid (PBAA);e.Polybutadiene — Acrylic Acid — Acrylonitrile (PBAN) (CAS 25265-19-4 / CAS 68891-50-9);f.Polytetrahydrofuran polyethylene glycol (TPEG).Technical Note:Polytetrahydrofuran polyethylene glycol (TPEG) is a block co-polymer of poly 1,4-Butanediol (CAS 110-63-4) and polyethylene glycol (PEG) (CAS 25322-68-3).g.Polyglycidyl nitrate (PGN or poly-GLYN) (CAS 27814-48-8)
	c.Other propellant additives and agents:
	1.SEE MILITARY GOODS CONTROLS FORCarboranes, decaboranes, pentaboranes and derivatives thereof;	M4C6c1	Carboranes, decaboranes, pentaboranes and derivatives thereof
	2.Triethylene glycol dinitrate (TEGDN) (CAS 111-22-8);	M4C6d1	Triethylene glycol dinitrate (TEGDN) (CAS 111-22-8);
	3.2-Nitrodiphenylamine (CAS 119-75-5);	M4C6e1	2-Nitrodiphenylamine (CAS 119-75-5);
	4.Trimethylolethane trinitrate (TMETN) (CAS 3032-55-1);	M4C6d2	Trimethylolethane trinitrate (TMETN) (CAS 3032-55-1);
	5.Diethylene glycol dinitrate (DEGDN) (CAS 693-21-0);	M4C6d4	Diethylene glycol dinitrate (DEGDN) (CAS 693-21-0)
	6.Ferrocene derivatives as follows:a.See Military Goods Controls for catocene;b.See Military Goods Controls for Ethyl ferrocene;c.See Military Goods Controls for Propyl ferrocene;d.See Military Goods Controls for n-butyl ferrocene;e.See Military Goods Controls for Pentyl ferrocene;f.See Military Goods Controls for Dicyclopentyl ferrocene;g.See Military Goods Controls for Dicyclohexyl ferrocene;h.See Military Goods Controls for Diethyl ferrocene;i.See Military Goods Controls for Dipropyl ferrocene;j.See Military Goods Controls for Dibutyl ferrocene;k.See Military Goods Controls for Dihexyl ferrocene;l.See Military Goods Controls for Acetyl ferrocene / 1,1′-diacetyl ferrocene;m.See Military Goods Controls for ferrocene carboxylic acids;n.See Military Goods Controls for butacene;o.Other ferrocene derivatives usable as rocket propellant burning rate modifiers, other than those specified in the Military Goods Controls.Note:1C111.c.6.o. does not control ferrocene derivatives that contain a six carbon aromatic functional group attached to the ferrocene molecule.	M4C6c2	Ferrocene derivatives, as follows:a.Catocene (CAS 37206-42-1);b.Ethyl ferrocene (CAS 1273-89-8);c.Propyl ferrocene;d.n-Butyl ferrocene (CAS 31904-29-7);e.Pentyl ferrocene (CAS 1274-00-6);f.Dicyclopentyl ferrocene (CAS 125861-17-8);g.Dicyclohexyl ferrocene;h.Diethyl ferrocene (CAS 1273-97-8);i.Dipropyl ferrocene;j.Dibutyl ferrocene (CAS 1274-08-4);k.Dihexyl ferrocene (CAS 93894-59-8);l.Acetyl ferrocene (CAS 1271-55-2) / 1,1′-diacetyl ferrocene (CAS 1273-94-5);m.Ferrocene carboxylic acid (CAS 1271-42-7) / 1,1′- Ferrocenedicarboxylic acid (CAS 1293-87-4);n.Butacene (CAS 125856-62-4);o.Other ferrocene derivatives usable as rocket propellant burning rate modifiers;Note:Item 4.C.6.c.2.o does not control ferrocene derivatives that contain a six carbon aromatic functional group attached to the ferrocene molecule.
	7.4,5 diazidomethyl-2-methyl-1,2,3-triazole (iso- DAMTR), other than that specified in the Military Goods Controls.Note:For propellants and constituent chemicals for propellants not specified in 1C111, see the Military Goods Controls.	M4C6d5	4,5 diazidomethyl-2-methyl-1,2,3-triazole (iso- DAMTR);
1C116	Maraging steels, useable in "missiles", having all of the following:N.B.:SEE ALSO 1C216.	M6C8	Maraging steels, usable in the systems specified in 1.A. or 19.A.1., having all of the following:a.Having an ultimate tensile strength, measured at 20 °C, equal to or greater than:1.0,9 GPa in the solution annealed stage; or2.1,5 GPa in the precipitation hardened stage; andb.Any of the following forms:1.Sheet, plate or tubing with a wall or plate thickness equal to or less than 5,0 mm; or2.Tubular forms with a wall thickness equal to or less than 50 mm and having an inner diameter equal to or greater than 270 mm.Technical Note:Maraging steels are iron alloys:a.Generally characterised by high nickel, very low carbon content and use substitutional elements or precipitates to produce strengthening and agehardening of the alloy; andb.Subjected to heat treatment cycles to facilitate the martensitic transformation process (solution annealed stage) and subsequently age hardened (precipitation hardened stage).
1C117	Materials for the fabrication of "missiles" components as follows:a.Tungsten and alloys in particulate form with a tungsten content of 97 % by weight or more and a particle size of 50 × 10-6 m (50 μm) or less;b.Molybdenum and alloys in particulate form with a molybdenum content of 97 % by weight or more and a particle size of 50 × 10-6 m (50 μm) or less;c.Tungsten materials in solid form having all of the following:1.Any of the following material compositions:a.Tungsten and alloys containing 97 % by weight or more of tungsten;b.Copper infiltrated tungsten containing 80 % by weight or more of tungsten; orc.Silver infiltrated tungsten containing 80 % by weight ot more of tungsten; and2.Able to be machined to any of the following products:a.Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater;b.Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; orc.Blocks having a size of 120 mm by 120 mm by 50 mm or greater.Technical Note:In 1C117 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M6C7	Materials for the fabrication of missile components in the systems specified in 1.A., 19.A.1. or 19.A.2, as follows:.a.Tungsten and alloys in particulate form with a tungsten content of 97 % by weight or more and a particle size of 50 × 10-6 m (50 μm) or less;b.Molybdenum and alloys in particulate form with a molybdenum content of 97 % by weight or more and a particle size of 50 × 10-6 m (50 μm) or less;c.Tungsten materials in the solid form having all of the following:1.Any of the following material compositions: i. Tungsten and alloys containing 97 % by weight or more of tungsten; ii. Copper infiltrated tungsten containing 80 % by weight or more of tungsten; or iii. Silver infiltrated tungsten containing 80 % by weight or more of tungsten; and2.Able to be machined to any of the following products: i. Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater; ii. Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; or iii. Blocks having a size of 120 mm × 120 mm × 50 mm or greater
1C118	Titanium-stabilised duplex stainless steel (Ti-DSS) having all of the following:a.Having all of the following characteristics:1.Containing 17,0 – 23,0 weight percent chromium and 4,5 – 7,0 weight percent nickel;2.Having a titanium content of greater than 0,10 weight percent; and3.A ferritic-austenitic microstructure (also referred to as a two-phase microstructure) of which at least 10 percent is austenite by volume (according to ASTM E-1181-87 or national equivalents); andb.Having any of the following forms:1.Ingots or bars having a size of 100 mm or more in each dimension;2.Sheets having a width of 600 mm or more and a thickness of 3 mm or less; or3.Tubes having an outer diameter of 600 mm or more and a wall thickness of 3 mm or less.	M6C9	Titanium-stabilized duplex stainless steel (Ti-DSS) usable in the systems specified in 1.A. or 19.A.1. and having all of the following:a.Having all of the following characteristics:1.Containing 17,0 – 23,0 weight percent chromium and 4,5 – 7,0 weight percent nickel;2.Having a titanium content of greater than 0,10 weight percent; and3.A ferritic-austenitic microstructure (also referred to as a two-phase microstructure ) of which at least 10 % is austenite by volume (according to ASTM E-1181-87 or national equivalents); andb.Any of the following forms:1.Ingots or bars having a size of 100 mm or more in each dimension;2.Sheets having a width of 600 mm or more and a thickness of 3 mm or less; or3.Tubes having an outer diameter of 600 mm or more and a wall thickness of 3 mm or less.
1C238	Chlorine trifluoride (ClF3).	M4C4a6	Compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen;Note:Item 4.C.4.a.6. does not control Nitrogen Trifluoride (NF3) (CAS 7783-54- 2) in a gaseous state as it is not usable for missile applications.

1DSoftware

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
1D001	"Software" specially designed or modified for the "development", "production" or "use" of equipment specified in 1B001 to 1B003.	M6D1	"Software" specially designed or modified for the operation or maintenance of equipment specified in 6.B.1.
1D101	"Software" specially designed or modified for the operation or maintenance of goods specified in1B101, 1B102, 1B115, 1B117, 1B118 or 1B119.	M4D1	"Software" specially designed or modified for the operation or maintenance of equipment specified in 4.B. for the "production" and handling of materials specified in 4.C.
		M6D1	"Software" specially designed or modified for the operation or maintenance of equipment specified in 6.B.1.
1D103	"Software" specially designed for analysis of reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures.	M17D1	"Software" specially designed for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures (i.e. stealth technology), for applications usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A.Note:17.D.1. includes "software" specially designed for analysis of signature reduction.

1ETechnology

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
1E001	"Technology" according to the General Technology Note for the "development" or "production" of equipment or materials specified in 1A001.b., 1A001.c., 1A002 to 1A005, 1A006.b., 1A007, 1B or 1C.	M	"Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 1.A., 1.B., or 1.D.
1E101	"Technology" according to the General Technology Note for the "use" of goods specified in 1A102, 1B001, 1B101, 1B102, 1B115 to 1B119, 1C001, 1C101, 1C107, 1C111 to 1C118, 1D101 or 1D103.	M	"Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 1.A., 1.B., or 1.D.
1E102	"Technology" according to the General Technology Note for the "development" of "software" specified in 1D001, 1D101 or 1D103.	M6E1	"Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment, materials or "software" specified in 6.A., 6.B., 6.C. or 6.D.
		M17E1	"Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment, materials or "software" specified in 17.A., 17.B., 17.C. or 17.D.Note:17.E.1. includes databases specially designed for analysis of signature reduction
1E103	[M6E2]"Technology" for the regulation of temperature, pressure or atmosphere in autoclaves or hydroclaves, when used for the "production" of "composites" or partially processed "composites".	M6E2	"Technical data" (including processing conditions) and procedures for the regulation of temperature, pressures or atmosphere in autoclaves or hydroclaves when used for the production of composites or partially processed composites, usable for equipment or materials specified in 6.A. or 6.C
1E104	"Technology" relating to the "production" of pyrolytically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1573 K (1300 °C) to 3173 K (2900 °C) temperature range at pressures of 130 Pa to 20 kPa.Note:1E104 includes "technology" for the composition of precursor gases, flow-rates and process control schedules and parameters.	M6E1

CATEGORY 2 — MATERRIALS PROCESSING

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
2A001	Anti-friction bearings and bearing systems, as follows, and components therefor:N.B.:SEE ALSO 2A101.Note:2A001 does not control balls with tolerances specified by the manufacturer in accordance with ISO 3290 as grade 5 or worse.a.Ball bearings and solid roller bearings, having all tolerances specified by the manufacturer in accordance with ISO 492 Tolerance Class 4 (or national equivalents), or better, and having both rings and rolling elements (ISO 5593), made from monel or beryllium;Note:2A001.a. does not control tapered roller bearings.b.Not used;c.Active magnetic bearing systems using any of the following:1.Materials with flux densities of 2,0 T or greater and yield strengths greater than 414 MPa;2.All-electromagnetic 3D homopolar bias designs for actuators; or3.High temperature (450 K (177 °C) and above) position sensors.	M3A7	Radial ball bearings having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all the following characteristics:a)An inner ring bore diameter between 12 and 50 mm;b)An outer ring outside diameter between 25 and 100 mm; andc)A width between 10 and 20 mm.
2A101	Radial ball bearings, other than those specified in 2A001, having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all the following characteristics:a.An inner ring bore diameter between 12 mm and 50 mm;b.An outer ring outside diameter between 25 mm and 100 mm; andc.A width between 10 mm and 20 mm.	M3A7	Radial ball bearings having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all the following characteristics:a)An inner ring bore diameter between 12 and 50 mm;b)An outer ring outside diameter between 25 and 100 mm; andc)A width between 10 and 20 mm.
2B004	Hot "isostatic presses" having all of the following, and specially designed components and accessories therefor:N.B.:SEE ALSO 2B104 and 2B204.a.A controlled thermal environment within the closed cavity and a chamber cavity with an inside diameter of 406 mm or more; andb.Having any of the following:1.A maximum working pressure exceeding 207 MPa;2.A controlled thermal environment exceeding 1773 K (1500 °C); or3.A facility for hydrocarbon impregnation and removal of resultant gaseous degradation products.Technical Note:The inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.N.B.:For specially designed dies, moulds and tooling see 1B003, 9B009 and the Military Goods Controls.	M6B3	Isostatic presses having all of the following characteristics:a)Maximum working pressure equal to or greater than 69 MPa;b)Designed to achieve and maintain a controlled thermal environment of 600 °C or greater; andc)Possessing a chamber cavity with an inside diameter of 254 mm or greater.
2B009	Spin-forming machines and flow-forming machines, which, according to the manufacturer's technical specification, can be equipped with "numerical control" units or a computer control and having all of the following:N.B.:SEE ALSO 2B109 AND 2B209.a.Three or more axes which can be coordinated simultaneously for "contouring control"; andb.A roller force more than 60 kN.Technical Note:For the purpose of 2B009, machines combining the function of spin-forming and flow-forming are regarded as flow-forming machines.	M3B3	Flow-forming machines, and specially designed components therefor, which:a)According to the manufacturers technical specification can be equipped with numerical control units or a computer control, even when not equipped with such units at delivery; andb)Have more than two axes which can be co-ordinated simultaneously for contouring control.Note:This item does not include machines that are not usable in the "production" of propulsion components and equipment (e.g. motor cases) for systems specified in 1.A.Technical Note:Machines combining the function of spin-forming and flow-forming are, for the purpose of this item, regarded as flow-forming machines.
2B104	"Isostatic presses", other than those specified in 2B004, having all of the following:N.B.:SEE ALSO 2B204.a.Maximum working pressure of 69 MPa or greater;b.Designed to achieve and maintain a controlled thermal environment of 873 K (600 °C) or greater; andc.Possessing a chamber cavity with an inside diameter of 254 mm or greater.	M6B3	Isostatic presses having all of the following characteristics:a)Maximum working pressure equal to or greater than 69 MPa;b)Designed to achieve and maintain a controlled thermal environment of 600 °C or greater; andc)Possessing a chamber cavity with an inside diameter of 254 mm or greater.
2B105	Chemical vapour deposition (CVD) furnaces, other than those specified in 2B005.a., designed or modified for the densification of carbon-carbon composites.	M6B4	Chemical vapour deposition furnaces designed or modified for the densification of carbon-carbon composites.
2B109	Flow-forming machines, other than those specified in 2B009, and specially designed components as follows:N.B.:SEE ALSO 2B209.a.Flow-forming machines having all of the following:1.According to the manufacturer's technical specification, can be equipped with "numerical control" units or a computer control, even when not equipped with such units; and2.With more than two axes which can be coordinated simultaneously for "contouring control".b.Specially designed components for flow-forming machines specified in 2B009 or 2B109.a.Note:2B109 does not control machines that are not usable in the production of propulsion components and equipment (e.g. motor cases) for systems specified in 9A005, 9A007.a. or 9A105.a.Technical Note:Machines combining the function of spin-forming and flow-forming are for the purpose of 2B109 regarded as flow-forming machines.	M3B3	Flow-forming machines, and specially designed components therefor, which:a)According to the manufacturers technical specification can be equipped with numerical control units or a computer control, even when not equipped with such units at delivery; andb)Have more than two axes which can be co-ordinated simultaneously for contouring control.Note:This item does not include machines that are not usable in the "production" of propulsion components and equipment (e.g. motor cases) for systems specified in 1.A.Technical Note:Machines combining the function of spin-forming and flow-forming are, for the purpose of this item, regarded as flow-forming machines.
2B116	Vibration test systems, equipment and components therefor, as follows:a.Vibration test systems employing feedback or closed loop techniques and incorporating a digital controller, capable of vibrating a system at an acceleration equal to or greater than 10 g rms between 20 Hz and 2 kHz while imparting forces equal to or greater than 50 kN, measured "bare table";b.Digital controllers, combined with specially designed vibration test software, with a "real-time control bandwidth" greater than 5 kHz designed for use with vibration test systems specified in 2B116.a.;Technical Note:In 2B116.b., "real-time control bandwidth" means the maximum rate at which a controller can execute complete cycles of sampling, processing data and transmitting control signals.c.Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force equal to or greater than 50 kN, measured "bare table", and usable in vibration test systems specified in 2B116.a.;d.Test piece support structures and electronic units designed to combine multiple shaker units in a system capable of providing an effective combined force equal to or greater than 50 kN, measured "bare table", and usable in vibration systems specified in 2B116.a.Technical Note:In 2B116, "bare table" means a flat table, or surface, with no fixture or fittings.	M15B1	Vibration test equipment, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A. or 20.A., and components therefor, as follows:a)Vibration test systems employing feedback or closed loop techniques and incorporating a digital controller, capable of vibrating a system at an acceleration equal to or greater than 10 g rms between 20 Hz and 2 kHz while imparting forces equal to or greater than 50 kN, measured "bare table";b)Digital controllers, combined with specially designed vibration test "software", with a "real-time control bandwidth" greater than 5 kHz and designed for use with vibration test systems specified in 15.B.1.a.;Technical Note:"Real-time control bandwidth" is defined as the maximum rate at which a controller can execute complete cycles of sampling, processing data and transmitting control signals.c)Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force equal to or greater than 50 kN, measured "bare table", and usable in vibration test systems specified in 15.B.1.a.;d)Test piece support structures and electronic units designed to combine multiple shaker units into a complete shaker system capable of providing an effective combined force equal to or greater than 50 kN, measured "bare table", and usable in vibration test systems specified in 15.B.1.a.Technical Note:Vibration test systems incorporating a digital controller are those systems, the functions of which are, partly or entirely, automatically controlled by stored and digitally coded electrical signals.
2B117	Equipment and process controls, other than those specified in 2B004, 2B005.a., 2B104 or 2B105, designed or modified for densification and pyrolysis of structural composite rocket nozzles and reentry vehicle nose tips.	M6B5	Equipment and process controls, other than those specified in 6.B.3. or 6.B.4., designed or modified for densification and pyrolysis of structural composite rocket nozzles and re-entry vehicle nose tips.
2B119	Balancing machines and related equipment, as follows:N.B.:SEE ALSO 2B219a.Balancing machines having all the following characteristics:1.Not capable of balancing rotors/assemblies having a mass greater than 3 kg;2.Capable of balancing rotors/assemblies at speeds greater than 12500 rpm;3.Capable of correcting unbalance in two planes or more; and4.Capable of balancing to a residual specific unbalance of 0,2 g mm per kg of rotor mass;Note:2B119.a. does not control balancing machines designed or modified for dental or other medical equipment.	M9B2a	Equipment as follows:1.Balancing machines having all the following characteristics:1.Not capable of balancing rotors/assemblies having a mass greater than 3 kg;2.Capable of balancing rotors/assemblies at speeds greater than 12500 rpm;3.Capable of correcting unbalance in two planes or more; and4.Capable of balancing to a residual specific unbalance of 0,2 g mm per kg of rotor mass;
	b.Indicator heads designed or modified for use with machines specified in 2B119.a.Technical Note:Indicator heads are sometimes known as balancing instrumentation.	M9B2b	Indicator heads (sometimes known as balancing instrumentation) designed or modified for use with machines specified in 9.B.2.a.;
2B120	Motion simulators or rate tables having all of the following characteristics:a.Two axes or more;b.Designed or modified to incorporate slip rings or integrated non-contact devices capable of transferring electrical power, signal information, or both; andc.Having any of the following characteristics:1.For any single axis having all of the following:a.Capable of rates of 400 degrees/s or more, or 30 degrees/s or less; andb.A rate resolution equal to or less than 6 degrees/s and an accuracy equal to or less than 0,6 degrees/s;2.Having a worst-case rate stability equal to or better (less) than plus or minus 0,05 % averaged over 10 degrees or more; or3.A positioning "accuracy" equal to or less (better) than 5 arc second.Note 1:2B120 does not control rotary tables designed or modified for machine tools or for medical equipment. For controls on machine tool rotary tables see 2B008.Note 2:Motion simulators or rate tables specified in 2B120 remain controlled whether or not slip rings or integrated non-contact devices are fitted at time of export.	M9B2c	Motion simulators/rate tables (equipment capable of simulating motion) having all of the following characteristics:1.Two axes or more;2.Designed or modified to incorporate sliprings or integrated non-contact devices capable of transferring electrical power, signal information, or both; and3.Having any of the following characteristics:a.For any single axis having all of the following:1.Capable of rates of 400 degrees/s or more, or 30 degrees/s or less; and2.A rate resolution equal to or less than 6 degrees/s and an accuracy equal to or less than 0,6 degrees/s;b.Having a worst-case rate stability equal to or better (less) than plus or minus 0,05 % averaged over 10 degrees or more; orc.A positioning "accuracy" equal to or less (better) than 5 arc second.
2B121	Positioning tables (equipment capable of precise rotary positioning in any axes), other than those specified in 2B120, having all the following characteristics:a.Two axes or more; andb.A positioning "accuracy" equal to or less (better) than 5 arc second.Note:2B121 does not control rotary tables designed or modified for machine tools or for medical equipment. For controls on machine tool rotary tables see 2B008	M9B2d	Positioning tables (equipment capable of precise rotary positioning in any axes) having the following characteristics:1.Two axes or more; and2.A positioning "accuracy" equal to or less (better) than 5 arc second;
2B122	Centrifuges capable of imparting accelerations above 100 g and designed or modified to incorporate slip rings or integrated non-contact devices capable of transferring electrical power, signal information, or both.Note:Centrifuges specified in 2B122 remain controlled whether or not slip rings or integrated non-contact devices are fitted at time of export	M9B2e	Centrifuges capable of imparting accelerations above 100 g and designed or modified to incorporate sliprings or integrated non-contact devices capable of transferring electrical power, signal information, or both

2DSoftware

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
2D001	"Software", other than that specified in 2D002, as follows:a."Software" specially designed or modified for the "development" or "production" of equipment specified in 2A001 or 2B001b."Software" specially designed or modified for the "use" of equipment specified in 2A001.c., 2B001 or 2B003 to 2B009.Note:2D001 does not control part programming "software" that generates "numerical control" codes for machining various parts.	M3D	SOFTWARE
2D101	"Software" specially designed or modified for the "use" of equipment specified in 2B104, 2B105, 2B109, 2B116, 2B117 or 2B119 to 2B122.N.B.:SEE ALSO 9D004.	M3D1	"Software" specially designed or modified for the "use" of "production facilities" and flow-forming machines specified in 3.B.1. or 3.B.3.
		M6D2	"Software" specially designed or modified for the equipment specified in 6.B.3., 6.B.4. or 6.B.5.
		M15D1	"Software" specially designed or modified for the "use" of equipment specified in 15.B. usable for testing systems specified in 1.A., 19.A.1. or 19.A.2. or subsystems specified in 2.A. or 20.A.

2ETechnology

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
2E001	"Technology" according to the General Technology Note for the "development" of equipment or "software" specified in 2A, 2B or 2D.Note:2E001 includes "technology" for the integration of probe systems into coordinate measurement machines specified in 2B006.a.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
2E002	"Technology" according to the General Technology Note for the "production" of equipment specified in 2A or 2B.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
2E101	"Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 2B004, 2B009, 2B104, 2B109, 2B116, 2B119 to 2B122 or 2D101.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".

CATEGORY 3 — ELECTRONICS3ASystems, Equipment and Components

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
3A001	Electronic components and specially designed components therefor, as follows:a.General purpose integrated circuits, as follows:Note 1:The control status of wafers (finished or unfinished), in which the function has been determined, is to be evaluated against the parameters of 3A001.a.Note 2:Integrated circuits include the following types:"Monolithic integrated circuits";"Hybrid integrated circuits";"Multichip integrated circuits";"Film type integrated circuits", including silicon-on-sapphire integrated circuits;"Optical integrated circuits";"Three dimensional integrated circuits".
	1.Integrated circuits designed or rated as radiation hardened to withstand any of the following:a.A total dose of 5 × 103 Gy (silicon) or higher;b.A dose rate upset of 5 × 106 Gy (silicon)/s or higher; orc.A fluence (integrated flux) of neutrons (1 MeV equivalent) of 5 × 1013 n/cm2 or higher on silicon, or its equivalent for other materials;Note:3A001.a.1.c. does not control Metal Insulator Semiconductors (MIS).	M18A1	"Radiation Hardened" "microcircuits" usable in protecting rocket systems and unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for the systems specified in 1.A.
		M18A2	"Detectors" specially designed or modified to protect rocket systems and unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for the systems specified in 1.A.Technical Note:A "detector" is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material. This includes devices that sense by one time operation or failure.
3A101	Electronic equipment, devices and components, other than those specified in 3A001, as follows:a.Analogue-to-digital converters, usable in "missiles", designed to meet military specifications for ruggedized equipment;	M14A1	Analogue-to-digital converters, usable in the systems specified in 1.A., having any of the following characteristics:a)Designed to meet military specifications for ruggedised equipment; orb)Designed or modified for military use and being any of the following types:
		M14A1b1	1.Analogue-to-digital converter "microcircuits", which are "radiation hardened" or have all of the following characteristics:a.Rated for operation in the temperature range from below –54 °C to above +125 °C; andb.Hermetically sealed; or
		M14A1b2	2.Electrical input type analogue-to-digital converter printed circuit boards or modules, having all of the following characteristics:a.Rated for operation in the temperature range from below –45 °C to above +80 °C; andb.Incorporating "microcircuits" specified in 14.A.1.b.1.
	b.Accelerators capable of delivering electromagnetic radiation produced by bremsstrahlung from accelerated electrons of 2 MeV or greater, and systems containing those accelerators.Note:3A101.b. above does not specify equipment specially designed for medical purposes.	M15B5	Accelerators capable of delivering electromagnetic radiation produced by bremsstrahlung from accelerated electrons of 2 MeV or greater, and equipment containing those accelerators, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A. or 20.A.Note:15.B.5. does not control equipment specially designed for medical purposes.Technical Note:In Item 15.B. "bare table" means a flat table, or surface, with no fixture or fittings.
3A102	"Thermal batteries" designed or modified for "missiles".Technical Notes:1.In 3A102 "thermal batteries" are single use batteries that contain a solid non-conducting inorganic salt as the electrolyte. These batteries incorporate a pyrolytic material that, when ignited, melts the electrolyte and activates the battery.2.In 3A102 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M12A6	Thermal batteries designed or modified for the systems specified in 1.A., 19.A.1. or 19.A.2.Note:Item 12.A.6. does not control thermal batteries specially designed for rocket systems or unmanned aerial vehicles that are not capable of a "range" equal to or greater than 300 km.Technical Note:Thermal batteries are single use batteries that contain a solid non-conducting inorganic salt as the electrolyte. These batteries incorporate a pyrolytic material that, when ignited, melts the electrolyte and activates the battery.

3DSoftware

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
3D101	"Software" specially designed or modified for the "use" of equipment specified in 3A101.b.	M15D1	"Software" specially designed or modified for the "use" of equipment specified in 3A101.b.

3ETechnology

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
3E001	"Technology" according to the General Technology Note for the "development" or "production" of equipment or materials specified in 3A, 3B or 3C;Note 1:3E001 does not control "technology" for the "production" of equipment or components controlled by 3A003.Note 2:3E001 does not control "technology" for the "development" or "production" of integrated circuits specified in 3A001.a.3. to 3A001.a.12., having all of the following:a.Using "technology" at or above 0,130 μm; andb.Incorporating multi-layer structures with three or fewer metal layers.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
3E101	"Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 3A001.a.1. or 2., 3A101, 3A102 or 3D101.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
3E102	"Technology" according to the General Technology Note for the "development" of "software" specified in 3D101.	M15E1	"Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 15.B. or 15.D.

CATEGORY 4 — COMPUTERS4ASystems, Equipment and Components

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
4A001	Electronic computers and related equipment, having any of the following and "electronic assemblies" and specially designed components therefor:N.B.:SEE ALSO 4A101.
	a.Specially designed to have any of the following:1.Rated for operation at an ambient temperature below 228 K (–45 °C) or above 358 K (85 °C); orNote:4A001.a.1. does not control computers specially designed for civil automobile, railway train or "civil aircraft" applications.2.Radiation hardened to exceed any of the following specifications:a.Total Dose 5 × 103 Gy (silicon);b.Dose Rate Upset 5 × 106 Gy (silicon)/s; orc.Single Event Upset 1 × 10–8 Error/bit/day;Note:4A001.a.2. does not control computers specially designed for "civil aircraft" applications.b.Not used.	M13A1	Analogue computers, digital computers or digital differential analysers, designed or modified for use in the systems specified in 1.A., having any of the following characteristics:a)Rated for continuous operation at temperatures from below –45 °C to above +55 °C; orb)Designed as ruggedised or "radiation hardened".
4A003	"Digital computers", "electronic assemblies", and related equipment therefor, as follows and specially designed components therefor:Note 1:4A003 includes the following:"Vector processors";Array processors;Digital signal processors;Logic processors;Equipment designed for "image enhancement";Equipment designed for "signal processing".Note 2:The control status of the "digital computers" and related equipment described in 4A003 is determined by the control status of other equipment or systems provided:a.The "digital computers" or related equipment are essential for the operation of the other equipment or systems;b.The "digital computers" or related equipment are not a "principal element" of the other equipment or systems; andN.B. 1:The control status of "signal processing" or "image enhancement" equipment specially designed for other equipment with functions limited to those required for the other equipment is determined by the control status of the other equipment even if it exceeds the "principal element" criterion.N.B. 2:For the control status of "digital computers" or related equipment for telecommunications equipment, see Category 5, Part 1 (Telecommunications).c.The "technology" for the "digital computers" and related equipment is determined by 4E.d.Not used
	e.Equipment performing analogue-to-digital conversions exceeding the limits specified in 3A001.a.5.;	M14A1b2	Electrical input type analogue-to-digital converter printed circuit boards or modules, having all of the following characteristics:a)Rated for operation in the temperature range from below –45 °C to above +80 °C; andb)Incorporating "microcircuits" specified in 14.A.1.b.1.
4A101	Analogue computers, "digital computers" or digital differential analysers, other than those specified in 4A001.a.1., which are ruggedized and designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.	M13A1b	Designed as ruggedised or "radiation hardened".
4A102	"Hybrid computers" specially designed for modelling, simulation or design integration of space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.Note:This control only applies when the equipment is supplied with "software" specified in 7D103 or 9D103.	M16A1	Specially designed hybrid (combined analogue/digital) computers for modelling, simulation or design integration of systems specified in 1.A. or the subsystems specified in 2.A.Note:This control only applies when the equipment is supplied with "software" specified in 16.D.1.

4ETechnology

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
4E001	a."Technology" according to the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 4A or 4D.b."Technology", other than that specified in 4E001.a., specially designed or modified for the "development" or "production" of equipment as follows:1."Digital computers" having an "Adjusted Peak Performance" ("APP") exceeding 1,0 Weighted TeraFLOPS (WT);2."Electronic assemblies" specially designed or modified for enhancing performance by aggregation of processors so that the "APP" of the aggregation exceeds the limit in 4E001.b.1.c."Technology" for the "development" of "intrusion software".	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".

CATEGORY 5 — TELECOMMUNICATIONS AND "INFORMATION SECURITY"Part 1 — Telecommunications5A1Systems, Equipment and Components

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
5A101	Telemetry and telecontrol equipment, including ground equipment, designed or modified for "missiles".Technical Note:In 5A101 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.Note:5A101 does not control:a.Equipment designed or modified for manned aircraft or satellites;b.Ground based equipment designed or modified for terrestrial or marine applications;c.Equipment designed for commercial, civil or "Safety of Life" (e.g. data integrity, flight safety) GNSS services;	M12A4	Telemetry and telecontrol equipment, including ground equipment, designed or modified for systems specified in 1.A., 19.A.1. or 19.A.2.Notes:1.12.A.4. does not control equipment designed or modified for manned aircraft or satellites.2.12.A.4. does not control ground based equipment designed or modified for terrestrial or marine applications.3.12.A.4. does not control equipment designed for commercial, civil or "Safety of Life" (e.g. data integrity, flight safety) GNSS services.

5D1Software

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
5D101	"Software" specially designed or modified for the "use" of equipment specified in 5A101.	M12D3	"Software" specially designed or modified for the "use" of equipment specified in 12.A.4. or 12.A.5., usable for systems specified in 1.A., 19.A.1. or 19.A.2.

5E1Technology

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
5E101	"Technology" according to the General Technology Note for the "development", "production" or "use" of equipment specified in 5A101.	M12E1	"Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 12.A. or 12.D.

CATEGORY 6 — SENSORS AND LASERS6ASystems, Equipment and Components

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
6A002	Optical sensors or equipment and components therefor, as follows:N.B.:SEE ALSO 6A102.a.Optical detectors as follows:1."Space-qualified" solid-state detectors as follows:Note:For the purpose of 6A002.a.1., solid-state detectors include "focal plane arrays".a."Space-qualified" solid-state detectors having all of the following:1.A peak response in the wavelength range exceeding 10 nm but not exceeding 300 nm; and2.A response of less than 0,1 % relative to the peak response at a wavelength exceeding 400 nm;	M18A2	"Detectors" specially designed or modified to protect rocket systems and unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for the systems specified in 1.A.Technical Note:A "detector" is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material. This includes devices that sense by one time operation or failure
	b."Space-qualified" solid-state detectors having all of the following:1.A peak response in the wavelength range exceeding 900 nm but not exceeding 1200 nm; and2.A response "time constant" of 95 ns or less;c."Space-qualified" solid-state detectors having a peak response in the wavelength range exceeding 1200 nm but not exceeding 30000 nm;d."Space-qualified" "focal plane arrays" having more than 2048 elements per array and having a peak response in the wavelength range exceeding 300 nm but not exceeding 900 nm.	M11A2	Passive sensors for determining bearings to specific electromagnetic sources (direction finding equipment) or terrain characteristics, designed or modified for use in the systems specified in 1.A.
6A006	"Magnetometers", "magnetic gradiometers", "intrinsic magnetic gradiometers", underwater electric field sensors, "compensation systems", and specially designed components therefor, as follows:N.B.:SEE ALSO 7A103.d.Note:6A006 does not control instruments specially designed for fishery applications or biomagnetic measurements for medical diagnostics.a."Magnetometers" and subsystems as follows:1."Magnetometers" using "superconductive" (SQUID) "technology" and having any of the following:a.SQUID systems designed for stationary operation, without specially designed subsystems designed to reduce in-motion noise, and having a "sensitivity" equal to or lower (better) than 50 fT (rms) per square root Hz at a frequency of 1 Hz; orb.SQUID systems having an in-motion-magnetometer "sensitivity" lower (better) than 20 pT (rms) per square root Hz at a frequency of 1 Hz and specially designed to reduce in-motion noise;2."Magnetometers" using optically pumped or nuclear precession (proton/Overhauser) "technology" having a "sensitivity" lower (better) than 20 pT (rms) per square root Hz at a frequency of 1 Hz;3."Magnetometers" using fluxgate "technology" having a "sensitivity" equal to or lower (better) than 10 pT (rms) per square root Hz at a frequency of 1 Hz;4.Induction coil "magnetometers" having a "sensitivity" lower (better) than any of the following:a.0,05 nT (rms) per square root Hz at frequencies of less than 1 Hz;b.1 × 10–3 nT (rms) per square root Hz at frequencies of 1 Hz or more but not exceeding 10 Hz; orc.1 × 10–4 nT (rms) per square root Hz at frequencies exceeding 10 Hz;5.Fibre optic "magnetometers" having a "sensitivity" lower (better) than 1 nT (rms) per square root Hz;b.Underwater electric field sensors having a "sensitivity" lower (better) than 8 nanovolt per metre per square root Hz when measured at 1 Hz;c."Magnetic gradiometers" as follows:1."Magnetic gradiometers" using multiple "magnetometers" specified in 6A006.a.;2.Fibre optic "intrinsic magnetic gradiometers" having a magnetic gradient field "sensitivity" lower (better) than 0,3 nT/m rms per square root Hz;3."Intrinsic magnetic gradiometers", using "technology" other than fibre-optic "technology", having a magnetic gradient field "sensitivity" lower (better) than 0,015 nT/m rms per square root Hz;d."Compensation systems" for magnetic or underwater electric field sensors resulting in a performance equal to or better than the specified parameters of 6A006.a., 6A006.b. or 6A006.c.;	M9A8	Three axis magnetic heading sensors having all of the following characteristics, and specially designed components therefor:a)Internal tilt compensation in pitch (+/– 90 degrees) and having roll (+/– 180 degrees) axes.b)Capable of providing azimuthal accuracy better (less) than 0,5 degrees rms at latitudes of +/– 80 degrees, referenced to local magnetic field; andc)Designed or modified to be integrated with flight control and navigation systems.Note:Flight control and navigation systems in Item 9.A.8. include gyrostabilisers, automatic pilots and inertial navigation systems.
6A007	Gravity meters (gravimeters) and gravity gradiometers, as follows:N.B.:SEE ALSO 6A107.a.Gravity meters designed or modified for ground use and having a static accuracy of less (better) than 10 μGal;Note:6A007.a. does not control ground gravity meters of the quartz element (Worden) type.b.Gravity meters designed for mobile platforms and having all of the following:1.A static accuracy of less (better) than 0,7 mGal; and2.An in-service (operational) accuracy of less (better) than 0,7 mGal having a "time-to-steady-state registration" of less than 2 minutes under any combination of attendant corrective compensations and motional influences;Technical Note:For the purposes of 6A007.b., "time-to-steady-state registration" (also referred to as the gravimeter's response time) is the time over which the disturbing effects of platform induced accelerations (high frequency noise) are reduced.c.Gravity gradiometers.	M12A3	Gravity meters (gravimeters) or gravity gradiometers, designed or modified for airborne or marine use, usable for systems specified in 1.A., as follows, and specially designed components therefor:a)Gravity meters having all the following:1.A static or operational accuracy equal to or less (better) than 0,7 milligal (mgal); and2.A time to steady-state registration of two minutes or less;b)Gravity gradiometers.
6A008	Radar systems, equipment and assemblies, having any of the following, and specially designed components therefor:N.B.:SEE ALSO 6A108.Note:6A008 does not control:Secondary surveillance radar (SSR);Civil Automotive Radar;Displays or monitors used for air traffic control (ATC);Meteorological (weather) radar;Precision approach radar (PAR) equipment conforming to ICAO standards and employing electronically steerable linear (1-dimensional) arrays or mechanically positioned passive antennae.	M11A1	Radar and laser radar systems, including altimeters, designed or modified for use in the systems specified in 1.A.Technical Note:Laser radar systems embody specialised transmission, scanning, receiving and signal processing techniques for utilisation of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics.
	a.Operating at frequencies from 40 GHz to 230 GHz and having any of the following:1.An average output power exceeding 100 mW; or2.Locating accuracy of 1 m or less (better) in range and 0,2 degree or less (better) in azimuth;b.A tunable bandwidth exceeding ± 6,25 % of the "centre operating frequency";Technical Note:The "centre operating frequency" equals one half of the sum of the highest plus the lowest specified operating frequencies.c.Capable of operating simultaneously on more than two carrier frequencies;	M12A5b	Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities:1.Angular resolution better than 1,5 mrad;2.Range of 30 km or greater with a range resolution better than 10 m rms; and3.Velocity resolution better than 3 m/s.
6A102	Radiation hardened "detectors", other than those specified in 6A002, specially designed modified for protecting against nuclear effects (e.g. electromagnetic pulse (EMP), X-rays, combined blast and thermal effects) and usable for "missiles", designed or rated to withstand radiation levels which meet or exceed a total irradiation dose of 5 × 105 rads (silicon).Technical Note:In 6A102, a "detector" is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material. This includes devices that sense by one time operation or failure.	M18A2	"Detectors" specially designed or modified to protect rocket systems and unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for the systems specified in 1.A.Technical Note:A "detector" is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material. This includes devices that sense by one time operation or failure.
6A107	Gravity meters (gravimeters) and components for gravity meters and gravity gradiometers, as follows:a.Gravity meters, other than those specified in 6A007.b, designed or modified for airborne or marine use, and having a static or operational accuracy equal to or less (better) than 0,7 milligal (mgal), and having a time-to-steady-state registration of two minutes or less;b.Specially designed components for gravity meters specified in 6A007.b or 6A107.a. and gravity gradiometers specified in 6A007.c.	M12A3	Gravity meters (gravimeters) or gravity gradiometers, designed or modified for airborne or marine use, usable for systems specified in 1.A., as follows, and specially designed components therefor:a)Gravity meters having all the following:1.A static or operational accuracy equal to or less (better) than 0,7 milligal (mgal); and2.A time to steady-state registration of two minutes or less;b)Gravity gradiometers.
6A108	Radar systems and tracking systems, other than those specified in entry 6A008, as follows:a.Radar and laser radar systems designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;Note:6A108.a. includes the following:a.Terrain contour mapping equipment;b.Imaging sensor equipment;c.Scene mapping and correlation (both digital and analogue) equipment;d.Doppler navigation radar equipment.	M11A1	Radar and laser radar systems, including altimeters, designed or modified for use in the systems specified in 1.A.Technical Note:Laser radar systems embody specialised transmission, scanning, receiving and signal processing techniques for utilisation of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics.
	b.Precision tracking systems, usable for "missiles", as follows:1.Tracking systems which use a code translator in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurements of in-flight position and velocity;2.Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities:a.Angular resolution better than 1,5 milliradians;b.Range of 30 km or greater with a range resolution better than 10 m rms;c.Velocity resolution better than 3 m/s.Technical Note:In 6A108.b. "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M12A5	Precision tracking systems, usable for systems specified in 1.A., 19.A.1. or 19.A.2. as follows:a.Tracking systems which use a code translator installed on the rocket or unmanned aerial vehicle in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurements of inflight position and velocity;b.Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities:1.Angular resolution better than 1,5 mrad;2.Range of 30 km or greater with a range resolution better than 10 m rms; and3.Velocity resolution better than 3 m/s.

6BTest, Inspection and Production Equipment

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
6B008	Pulse radar cross-section measurement systems having transmit pulse widths of 100 ns or less, and specially designed components therefor.N.B.:SEE ALSO 6B108.	M17B1	Systems, specially designed for radar cross section measurement, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A
6B108	Systems, other than those specified in 6B008, specially designed for radar cross section measurement usable for "missiles" and their subsystems.Technical Note:In 6B108 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M17B1	Systems, specially designed for radar cross section measurement, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A

6DSoftware

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
6D002	"Software" specially designed for the "use" of equipment specified in 6A002.b., 6A008 or 6B008.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
6D102	"Software" specially designed or modified for the "use" of goods specified in 6A108.	M11D1	"Software" specially designed or modified for the "use" of equipment specified in 11.A.1., 11.A.2. or 11.A.4.
		M12D3	"Software" specially designed or modified for the "use" of equipment specified in 12.A.4. or 12.A.5., usable for systems specified in 1.A., 19.A.1. or 19.A.2.
6D103	"Software" which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for "missiles".Technical Note:In 6D103 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M12D2	"Software" which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for systems specified in 1.A., 19.A.1. or 19.A.2.

6ETechnology

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
6E001	"Technology" according to the General Technology Note for the "development" of equipment, materials or "software" specified in 6A, 6B, 6C or 6D.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
6E002	"Technology" according to the General Technology Note for the "production" of equipment or materials specified in 6A, 6B or 6C.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
6E101	"Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 6A002, 6A007.b. and c., 6A008, 6A102, 6A107, 6A108, 6B108, 6D102 or 6D103.Note:6E101 only specifies "technology" for equipment specified in 6A008 when it is designed for airborne applications and is usable in "missiles".	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".

CATEGORY 7 — NAVIGATION AND AVIONICS7ASystems, Equipment and Components

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
7A001	Accelerometers as follows and specially designed components therefor:N.B.:SEE ALSO 7A101.N.B.:For angular or rotational accelerometers, see 7A001.b.a.Linear accelerometers having any of the following:1.Specified to function at linear acceleration levels less than or equal to 15 g and having any of the following:a.A "bias" "stability" of less (better) than 130 micro g with respect to a fixed calibration value over a period of one year; orb.A "scale factor" "stability" of less (better) than 130 ppm with respect to a fixed calibration value over a period of one year;2.Specified to function at linear acceleration levels exceeding 15 g but less than or equal to 100 g and having all of the following:a.A "bias" "repeatability" of less (better) than 1250 micro g over a period of one year; andb.A "scale factor" "repeatability" of less (better) than 1250 ppm over a period of one year; or3.Designed for use in inertial navigation or guidance systems and specified to function at linear acceleration levels exceeding 100 g;Note:7A001.a.1. and 7A001.a.2. do not control accelerometers limited to measurement of only vibration or shock.	M9A3	Linear accelerometers, designed for use in inertial navigation systems or in guidance systems of all types, usable in the systems specified in 1.A., 19.A.1. or 19.A.2., having all of the following characteristics, and specially designed components therefor:a."Scale factor" "repeatability" less (better) than 1250 ppm; andb."Bias" "repeatability" less (better) than 1250 micro g.Note:Item 9.A.3. does not control accelerometers specially designed and developed as Measurement While Drilling (MWD) sensors for use in downhole well service operations.Technical Notes:1."Bias" is defined as the accelerometer output when no acceleration is applied.2."Scale factor" is defined as the ratio of change in output to a change in the input.3.The measurement of "bias" and "scale factor" refers to one sigma standard deviation with respect to a fixed calibration over a period of one year.4."Repeatability" is defined according to IEEE Standard for Inertial Sensor Terminology 528-2001 in the Definitions section paragraph 2.214 titled repeatability (gyro, accelerometer) as follows: "The closeness of agreement among repeated measurements of the same variable under the same operating conditions when changes in conditions or non-operating periods occur between measurements".
	b.Angular or rotational accelerometers, specified to function at linear acceleration levels exceeding 100 g.	M9A5	Accelerometers or gyros of any type, designed for use in inertial navigation systems or in guidance systems of all types, specified to function at acceleration levels greater than 100 g, and specially designed components therefor.Note:9.A.5. does not include accelerometers that are designed to measure vibration or shock.
7A002	Gyros or angular rate sensors, having any of the following and specially designed components therefor:N.B.:SEE ALSO 7A102.N.B.:For angular or rotational accelerometers, see 7A001.b.a.Specified to function at linear acceleration levels less than or equal to 100 g and having any of the following:1.A rate range of less than 500 degrees per second and having any of the following:a.A "bias" "stability" of less (better) than 0,5 degree per hour, when measured in a 1 g environment over a period of one month, and with respect to a fixed calibration value; orb.An "angle random walk" of less (better) than or equal to 0,0035 degree per square root hour; orNote:7A002.a.1.b. does not control "spinning mass gyros".2.A rate range greater than or equal to 500 degrees per second and having any of the following:a.A "bias" "stability" of less (better) than 4 degrees per hour, when measured in a 1 g environment over a period of three minutes, and with respect to a fixed calibration value; orb.An "angle random walk" of less (better) than or equal to 0,1 degree per square root hour; orNote:7A002.a.2.b. does not control "spinning mass gyros".	M9A4	All types of gyros usable in the systems specified in 1.A., 19.A.1 or 19.A.2., with a rated "drift rate" "stability" of less than 0,5 degrees (1 sigma or rms) per hour in a 1 g environment, and specially designed components therefor.Technical Notes:1."Drift rate" is defined as the component of gyro output that is functionally independent of input rotation and is expressed as an angular rate. (IEEE STD 528-2001 paragraph 2.56)2."Stability" is defined as a measure of the ability of a specific mechanism or performance coefficient to remain invariant when continuously exposed to a fixed operating condition. (This definition does not refer to dynamic or servo stability.) (IEEE STD 528-2001 paragraph 2.247)
	b.Specified to function at linear acceleration levels exceeding 100 g.	M9A5	Accelerometers or gyros of any type, designed for use in inertial navigation systems or in guidance systems of all types, specified to function at acceleration levels greater than 100 g, and specially designed components therefor.Note:9.A.5. does not include accelerometers that are designed to measure vibration or shock.
7A003	"Inertial measurement equipment or systems", having any of the following:N.B.:SEE ALSO 7A103.Note 1:"Inertial measurement equipment or systems" incorporate accelerometers or gyroscopes to measure changes in velocity and orientation in order to determine or maintain heading or position without requiring an external reference once aligned. "Inertial measurement equipment or systems" include:Attitude and Heading Reference Systems (AHRSs);Gyrocompasses;Inertial Measurement Units (IMUs);Inertial Navigation Systems (INSs);Inertial Reference Systems (IRSs);Inertial Reference Units (IRUs).Note 2:7A003 does not control "inertial measurement equipment or systems" which are certified for use on "civil aircraft" by civil aviation authorities of one or more "participating states".Technical Notes:1."Positional aiding references" independently provide position, and include:a.Global Navigation Satellite Systems (GNSS);b."Data-Based Referenced Navigation" ("DBRN").2."Circular Error Probable" ("CEP") — In a circular normal distribution, the radius of the circle containing 50 % of the individual measurements being made, or the radius of the circle within which there is a 50 % probability of being located.a.Designed for "aircraft", land vehicles or vessels, providing position without the use of "positional aiding references", and having any of the following accuracies subsequent to normal alignment:1.0,8 nautical miles per hour (nm/hr) "Circular Error Probable" ("CEP") rate or less (better);2.0,5 % distanced travelled "CEP" or less (better); or3.Total drift of 1 nautical mile "CEP" or less (better) in a 24 hr period;Technical Note:The performance parameters in 7A003.a.1., 7A003.a.2. and 7A003.a.3. typically apply to "inertial measurement equipment or systems" designed for "aircraft", vehicles and vessels, respectively. These parameters result from the utilisation of specialised non-positional aiding references (e.g., altimeter, odometer, velocity log). As a consequence, the specified performance values cannot be readily converted between these parameters. Equipment designed for multiple platforms are evaluated against each applicable entry 7A003.a.1., 7A003.a.2., or 7A003.a.3.b.Designed for "aircraft", land vehicles or vessels, with an embedded "positional aiding reference" and providing position after loss of all "positional aiding references" for a period of up to 4 minutes, having an accuracy of less (better) than 10 meters "CEP";Technical Note:7A003.b. refers to systems in which "inertial measurement equipment or systems" and other independent "positional aiding references" are built into a single unit (i.e., embedded) in order to achieve improved performance.c.Designed for "aircraft", land vehicles or vessels, providing heading or True North determination and having any of the following:1.A maximum operating angular rate less (lower) than 500 deg/s and a heading accuracy without the use of "positional aiding references" equal to or less (better) than 0,07 deg sec(Lat) (equivalent to 6 arc minutes rms at 45 degrees latitude); or2.A maximum operating angular rate equal to or greater (higher) than 500 deg/s and a heading accuracy without the use of "positional aiding references" equal to or less (better) than 0,2 deg sec(Lat) (equivalent to 17 arc minutes rms at 45 degrees latitude); ord.Providing acceleration measurements or angular rate measurements, in more than one dimension, and having any of the following:1.Performance specified by 7A001 or 7A002 along any axis, without the use of any aiding references; or2.Being "space-qualified" and providing angular rate measurements having an "angle random walk" along any axis of less (better) than or equal to 0,1 degree per square root hour.Note:7A003.d.2. does not control "inertial measurement equipment or systems" that contain "spinning mass gyros" as the only type of gyro.	M2A1d	"Guidance sets", usable in the systems specified in 1.A., capable of achieving system accuracy of 3,33 % or less of the "range" (e.g. a "CEP" of 10 km or less at a "range" of 300 km), except as provided in the Note below 2.A.1. for those designed for missiles with a "range" under 300 km or manned aircraft;
		M9A6	Inertial or other equipment using accelerometers specified in 9.A.3. or 9.A.5. or gyros specified in 9.A.4. or 9.A.5., and systems incorporating such equipment, and specially designed components therefor.
		M9A8	Three axis magnetic heading sensors having all of the following characteristics, and specially designed components therefor:a.Internal tilt compensation in pitch (+/– 90 degrees) and having roll (+/– 180 degrees) axes.b.Capable of providing azimuthal accuracy better (less) than 0,5 degrees rms at latitudes of +/– 80 degrees, referenced to local magnetic field; andc.Designed or modified to be integrated with flight control and navigation systems.Note:Flight control and navigation systems in Item 9.A.8. include gyrostabilisers, automatic pilots and inertial navigation systems.
7A004	"Star trackers" and components therefor, as follows:N.B.:SEE ALSO 7A104.a."Star trackers" with a specified azimuth accuracy of equal to or less (better) than 20 seconds of arc throughout the specified lifetime of the equipment;b.Components specially designed for equipment specified in 7A004.a. as follows:1.Optical heads or baffles;2.Data processing units.Technical Note:"Star trackers" are also referred to as stellar attitude sensors or gyro-astro compasses.	M9A2	Gyro-astro compasses and other devices which derive position or orientation by means of automatically tracking celestial bodies or satellites, and specially designed components therefor.
7A005	Global Navigation Satellite Systems (GNSS) receiving equipment having any of the following and specially designed components therefor:N.B.:SEE ALSO 7A105.N.B.:For equipment specially designed for military use, see Military Goods Controls.a.Employing a decryption algorithm specially designed or modified for government use to access the ranging code for position and time; orb.Employing "adaptive antenna systems".Note:7A005.b. does not control GNSS receiving equipment that only uses components designed to filter, switch, or combine signals from multiple omni-directional antennae that do not implement adaptive antenna techniques.Technical Note:For the purposes of 7A005.b "adaptive antenna systems" dynamically generate one or more spatial nulls in an antenna array pattern by signal processing in the time domain or frequency domain.	M11A3	Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, GLONASS or Galileo), having any of the following characteristics, and specially designed components therefor:a.Designed or modified for use in systems specified in 1.A.; orb.Designed or modified for airborne applications and having any of the following:1.Capable of providing navigation information at speeds in excess of 600 m/s;2.Employing decryption, designed or modified for military or governmental services, to gain access to GNSS secure signal/data; or3.Being specially designed to employ anti-jam features (e.g. null steering antenna or electronically steerable antenna) to function in an environment of active or passive countermeasures.Note:11.A.3.b.2. and 11.A.3.b.3. do not control equipment designed for commercial, civil or "Safety of Life" (e.g. data integrity, flight safety) GNSS services.
7A006	Airborne altimeters operating at frequencies other than 4,2 to 4,4 GHz inclusive and having any of the following:N.B.:SEE ALSO 7A106.a."Power management"; orb.Using phase shift key modulation.	M11A1	Radar and laser radar systems, including altimeters, designed or modified for use in the systems specified in 1.A.Technical Note:Laser radar systems embody specialised transmission, scanning, receiving and signal processing techniques for utilisation of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics.
7A101	Linear accelerometers, other than those specified in 7A001, designed for use in inertial navigation systems or in guidance systems of all types, usable in "missiles", having all the following characteristics, and specially designed components therefor:a.A "bias" "repeatability" of less (better) than 1250 micro g; andb.A "scale factor" "repeatability" of less (better) than 1250 ppm;Note:7A101 does not control accelerometers specially designed and developed as Measurement While Drilling (MWD) Sensors for use in downhole well service operations.Technical Notes:1.In 7A101 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km;2.In 7A101 the measurement of "bias" and "scale factor" refers to a one sigma standard deviation with respect to a fixed calibration over a period of one year;	M9A3	Linear accelerometers, designed for use in inertial navigation systems or in guidance systems of all types, usable in the systems specified in 1.A., 19.A.1. or 19.A.2., having all of the following characteristics, and specially designed components therefor:a."Scale factor" "repeatability" less (better) than 1250 ppm; andb."Bias" "repeatability" less (better) than 1250 micro g.Note:Item 9.A.3. does not control accelerometers specially designed and developed as Measurement While Drilling (MWD) sensors for use in downhole well service operations.Technical Notes:1."Bias" is defined as the accelerometer output when no acceleration is applied.2."Scale factor" is defined as the ratio of change in output to a change in the input.3.The measurement of "bias" and "scale factor" refers to one sigma standard deviation with respect to a fixed calibration over a period of one year.4."Repeatability" is defined according to IEEE Standard for Inertial Sensor Terminology 528-2001 in the Definitions section paragraph 2.214 titled repeatability (gyro, accelerometer) as follows: "The closeness of agreement among repeated measurements of the same variable under the same operating conditions when changes in conditions or non-operating periods occur between measurements".
7A102	All types of gyros, other than those specified in 7A002, usable in "missiles", with a rated "drift rate" "stability" of less than 0,5° (1 sigma or rms) per hour in a 1 g environment and specially designed components therefor.Technical Notes:1.In 7A102 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.2.In 7A102 "stability" is defined as a measure of the ability of a specific mechanism or performance coefficient to remain invariant when continuously exposed to a fixed operating condition (IEEE STD 528-2001 paragraph 2.247).	M9A4	All types of gyros usable in the systems specified in 1.A., 19.A.1 or 19.A.2., with a rated "drift rate" "stability" of less than 0,5 degrees (1 sigma or rms) per hour in a 1 g environment, and specially designed components therefor.Technical Notes:1."Drift rate" is defined as the component of gyro output that is functionally independent of input rotation and is expressed as an angular rate. (IEEE STD 528-2001 paragraph 2.56)2."Stability" is defined as a measure of the ability of a specific mechanism or performance coefficient to remain invariant when continuously exposed to a fixed operating condition. (This definition does not refer to dynamic or servo stability.) (IEEE STD 528-2001 paragraph 2.247)
7A103	Instrumentation, navigation equipment and systems, other than those specified in 7A003, as follows; and specially designed components therefor:a.Inertial or other equipment, using accelerometers or gyros as follows, and systems incorporating such equipment:1.Accelerometers specified in 7A001.a.3., 7A001.b. or 7A101 or gyros specified in 7A002 or 7A102; or2.Accelerometers specified in 7A001.a.1. or 7A001.a.2., designed for use in inertial navigation systems or in guidance systems of all types, and usable in "missiles";Note:7A103.a. does not specify equipment containing accelerometers specified in 7A001 where such accelerometers are specially designed and developed as MWD (Measurement While Drilling) sensors for use in down-hole well services operations.	M9A6	Inertial or other equipment using accelerometers specified in 9.A.3. or 9.A.5. or gyros specified in 9.A.4. or 9.A.5., and systems incorporating such equipment, and specially designed components therefor.
	b.Integrated flight instrument systems which include gyrostabilisers or automatic pilots, designed or modified for use in "missiles";	M9A1	Integrated flight instrument systems which include gyrostabilisers or automatic pilots, designed or modified for use in the systems specified in 1.A., or 19.A.1. or 19.A.2. and specially designed components therefor.
	c."Integrated navigation systems", designed or modified for "missiles" and capable of providing a navigational accuracy of 200 m Circle of Equal Probability (CEP) or less;Technical Note:An "integrated navigation system" typically incorporates the following components:1.An inertial measurement device (e.g., an attitude and heading reference system, inertial reference unit, or inertial navigation system);2.One or more external sensors used to update the position and/or velocity, either periodically or continuously throughout the flight (e.g., satellite navigation receiver, radar altimeter, and/or Doppler radar); and3.Integration hardware and software;	M9A7	"Integrated navigation systems", designed or modified for the systems specified in 1.A., 19.A.1. or 19.A.2. and capable of providing a navigational accuracy of 200 m CEP or less.Technical Note:An "integrated navigation system" typically incorporates all of the following components:a.An inertial measurement device (e.g. an attitude and heading reference system, inertial reference unit, or inertial navigation system);b.One or more external sensors used to update the position and/or velocity, either periodically or continuously throughout the flight (e.g. satellite navigation receiver, radar altimeter, and/or Doppler radar); andc.Integration hardware and software.N.B.For integration "software", see Item 9.D.4.
	d.Three axis magnetic heading sensors, designed or modified to be integrated with flight control and navigation systems, other than those specified in 6A006, having all the following characteristics, and specially designed components therefor;1.Internal tilt compensation in pitch (± 90 degrees) and roll (± 180 degrees) axes;2.Capable of providing azimuthal accuracy better (less) than 0,5 degrees rms at latitude of ± 80 degrees, reference to local magnetic field.Note:Flight control and navigation systems in 7A103.d. include gyrostabilizers, automatic pilots and inertial navigation systems.Technical Note:In 7A103 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M9A8	Three axis magnetic heading sensors having all of the following characteristics, and specially designed components therefor:a.Internal tilt compensation in pitch (+/– 90 degrees) and having roll (+/– 180 degrees) axes.b.Capable of providing azimuthal accuracy better (less) than 0,5 degrees rms at latitudes of +/– 80 degrees, referenced to local magnetic field; andc.Designed or modified to be integrated with flight control and navigation systems.Note:Flight control and navigation systems in Item 9.A.8. include gyrostabilisers, automatic pilots and inertial navigation systems.
7A104	Gyro-astro compasses and other devices, other than those specified in 7A004, which derive position or orientation by means of automatically tracking celestial bodies or satellites and specially designed components therefor.	M9A2	Gyro-astro compasses and other devices which derive position or orientation by means of automatically tracking celestial bodies or satellites, and specially designed components therefor.
7A105	Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, GLONASS, or Galileo), other than those specified in 7A005, having any of the following characteristics, and specially designed components therefor:a.Designed or modified for use in space launch vehicles specified in 9A004, sounding rockets specified in 9A104 or unmanned aerial vehicles specified in 9A012 or 9A112.a.; orb.Designed or modified for airborne applications and having any of the following:1.Capable of providing navigation information at speeds in excess of 600 m/s;2.Employing decryption, designed or modified for military or governmental services, to gain access to GNSS secured signal/data; or3.Being specially designed to employ anti-jam features (e.g. null steering antenna or electronically steerable antenna) to function in an environment of active or passive countermeasures.Note:7A105.b.2. and 7A105.b.3. do not control equipment designed for commercial, civil or "Safety of Life" (e.g., data integrity, flight safety) GNSS services.	M11A3	Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, GLONASS or Galileo), having any of the following characteristics, and specially designed components therefor:a.Designed or modified for use in systems specified in 1.A.; orb.Designed or modified for airborne applications and having any of the following:1.Capable of providing navigation information at speeds in excess of 600 m/s;2.Employing decryption, designed or modified for military or governmental services, to gain access to GNSS secure signal/data; or3.Being specially designed to employ anti-jam features (e.g. null steering antenna or electronically steerable antenna) to function in an environment of active or passive countermeasures.Note:11.A.3.b.2. and 11.A.3.b.3. do not control equipment designed for commercial, civil or "Safety of Life" (e.g. data integrity, flight safety) GNSS services.
7A106	Altimeters, other than those specified in 7A006, of radar or laser radar type, designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.	M11A1	Radar and laser radar systems, including altimeters, designed or modified for use in the systems specified in 1.A.Technical Note:Laser radar systems embody specialised transmission, scanning, receiving and signal processing techniques for utilisation of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics.
7A115	Passive sensors for determining bearing to specific electromagnetic source (direction finding equipment) or terrain characteristics, designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.Note:7A115 includes sensors for the following equipment:a.Terrain contour mapping equipment;b.Imaging sensor equipment (both active and passive);c.Passive interferometer equipment	M11A2	Passive sensors for determining bearings to specific electromagnetic sources (direction finding equipment) or terrain characteristics, designed or modified for use in the systems specified in 1.A.
7A116	Flight control systems and servo valves, as follows; designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.a.Hydraulic, mechanical, electro-optical, or electro-mechanical flight control systems (including fly-by-wire types);	M10A1	Pneumatic, hydraulic, mechanical, electro-optical, or electromechanical flight control systems (including fly-by-wire and fly-by-light systems) designed or modified for the systems specified in 1.A.
	b.Attitude control equipment;	M10A2	Attitude control equipment designed or modified for the systems specified in 1.A.
	c.Flight control servo valves designed or modified for the systems specified in 7A116.a. or 7A116.b., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz.	M10A3	Flight control servo valves designed or modified for the systems in 10.A.1. or 10.A.2., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz.Note:Systems, equipment or valves specified in 10.A. may be exported as part of a manned aircraft or satellite or in quantities appropriate for replacement parts for manned aircraft.
7A117	"Guidance sets", usable in "missiles" capable of achieving system accuracy of 3,33 % or less of the range (e.g., a "CEP" of 10 km or less at a range of 300 km).	M2A1d	"Guidance sets", usable in the systems specified in 1.A., capable of achieving system accuracy of 3,33 % or less of the "range" (e.g. a "CEP" of 10 km or less at a "range" of 300 km), except as provided in the Note below 2.A.1. for those designed for missiles with a "range" under 300 km or manned aircraft;

7BTest, Inspection and Production Equipment

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
7B001	Test, calibration or alignment equipment, specially designed for equipment specified in 7A.Note:7B001 does not control test, calibration or alignment equipment for "Maintenance Level I" or "Maintenance Level II".Technical Notes:1."Maintenance Level I"The failure of an inertial navigation unit is detected on the aircraft by indications from the Control and Display Unit (CDU) or by the status message from the corresponding sub-system. By following the manufacturer's manual, the cause of the failure may be localised at the level of the malfunctioning Line Replaceable Unit (LRU). The operator then removes the LRU and replaces it with a spare.2."Maintenance Level II"The defective LRU is sent to the maintenance workshop (the manufacturer's or that of the operator responsible for level II maintenance). At the maintenance workshop, the malfunctioning LRU is tested by various appropriate means to verify and localise the defective Shop Replaceable Assembly (SRA) module responsible for the failure. This SRA is removed and replaced by an operative spare. The defective SRA (or possibly the complete LRU) is then shipped to the manufacturer. "Maintenance Level II" does not include the disassembly or repair of controlled accelerometers or gyro sensors.	M2B2	"Production equipment" specially designed for the subsystems specified in 2.A.
		M9B1	"Production equipment", and other test, calibration and alignment equipment, other than that described in 9.B.2., designed or modified to be used with equipment specified in 9.A.Note:Equipment specified in 9.B.1. includes the following:a.For laser gyro equipment, the following equipment used to characterise mirrors, having the threshold accuracy shown or better:1.Scatterometer (10 ppm);2.Reflectometer (50 ppm);3.Profilometer (5 Angstroms);b.For other inertial equipment:1.Inertial Measurement Unit (IMU) Module Tester;2.IMU Platform Tester;3.IMU Stable Element Handling Fixture;4.IMU Platform Balance Fixture;5.Gyro Tuning Test Station;6.Gyro Dynamic Balance Station;7.Gyro Run-In/Motor Test Station;8.Gyro Evacuation and Filling Station;9.Centrifuge Fixture for Gyro Bearings;10.Accelerometer Axis Align Station;11.Accelerometer Test Station;12.Fibre Optic Gyro Coil Winding Machines
		M10B1	Test, calibration, and alignment equipment specially designed for equipment specified in 10.A.
7B002	Equipment specially designed to characterize mirrors for ring "laser" gyros, as follows:N.B.:SEE ALSO 7B102.a.Scatterometers having a measurement accuracy of 10 ppm or less (better);b.Profilometers having a measurement accuracy of 0,5 nm (5 angstrom) or less (better).	M9B1	"Production equipment", and other test, calibration and alignment equipment, other than that described in 9.B.2., designed or modified to be used with equipment specified in 9.A.Note:Equipment specified in 9.B.1. includes the following:a.For laser gyro equipment, the following equipment used to characterise mirrors, having the threshold accuracy shown or better:1.Scatterometer (10 ppm);2.Reflectometer (50 ppm);3.Profilometer (5 Angstroms);b.For other inertial equipment:1.Inertial Measurement Unit (IMU) Module Tester;2.IMU Platform Tester;3.IMU Stable Element Handling Fixture;4.IMU Platform Balance Fixture;5.Gyro Tuning Test Station;6.Gyro Dynamic Balance Station;7.Gyro Run-In/Motor Test Station;8.Gyro Evacuation and Filling Station;9.Centrifuge Fixture for Gyro Bearings;10.Accelerometer Axis Align Station;11.Accelerometer Test Station;12.Fibre Optic Gyro Coil Winding Machines.
7B003	Equipment specially designed for the "production" of equipment specified in 7A.Note:7B003 includes:Gyro tuning test stations;Gyro dynamic balance stations;Gyro run-in/motor test stations;Gyro evacuation and fill stations;Centrifuge fixtures for gyro bearings;Accelerometer axis align stations;Fibre optic gyro coil winding machines.	M2B2	"Production equipment" specially designed for the subsystems specified in 2.A.
		M9B1	"Production equipment", and other test, calibration and alignment equipment, other than that described in 9.B.2., designed or modified to be used with equipment specified in 9.A.Note:Equipment specified in 9.B.1. includes the following:a.For laser gyro equipment, the following equipment used to characterise mirrors, having the threshold accuracy shown or better:1.Scatterometer (10 ppm);2.Reflectometer (50 ppm);3.Profilometer (5 Angstroms);b.For other inertial equipment:1.Inertial Measurement Unit (IMU) Module Tester;2.IMU Platform Tester;3.IMU Stable Element Handling Fixture;4.IMU Platform Balance Fixture;5.Gyro Tuning Test Station;6.Gyro Dynamic Balance Station;7.Gyro Run-In/Motor Test Station;8.Gyro Evacuation and Filling Station;9.Centrifuge Fixture for Gyro Bearings;10.Accelerometer Axis Align Station;11.Accelerometer Test Station;12.Fibre Optic Gyro Coil Winding Machines.
7B102	Reflectometers specially designed to characterise mirrors, for "laser" gyros, having a measurement accuracy of 50 ppm or less (better).	M9B1	"Production equipment", and other test, calibration and alignment equipment, other than that described in 9.B.2., designed or modified to be used with equipment specified in 9.A.Note:Equipment specified in 9.B.1. includes the following:a.For laser gyro equipment, the following equipment used to characterise mirrors, having the threshold accuracy shown or better:1.Scatterometer (10 ppm);2.Reflectometer (50 ppm);3.Profilometer (5 Angstroms);b.For other inertial equipment:1.Inertial Measurement Unit (IMU) Module Tester;2.IMU Platform Tester;3.IMU Stable Element Handling Fixture;4.IMU Platform Balance Fixture;5.Gyro Tuning Test Station;6.Gyro Dynamic Balance Station;7.Gyro Run-In/Motor Test Station;8.Gyro Evacuation and Filling Station;9.Centrifuge Fixture for Gyro Bearings;10.Accelerometer Axis Align Station;11.Accelerometer Test Station;12.Fibre Optic Gyro Coil Winding Machines.
7B103	"Production facilities" and "production equipment" as follows:
	a."Production facilities" specially designed for equipment specified in 7A117;	M2B1	"Production facilities" specially designed for the subsystems specified in 2.A
	b."Production equipment", and other test, calibration and alignment equipment, other than that specified in 7B001 to 7B003, designed or modified to be used with equipment specified in 7A.	M2B2*	"Production equipment" specially designed for the subsystems specified in 2.A.
		M9B1	"Production equipment", and other test, calibration and alignment equipment, other than that described in 9.B.2., designed or modified to be used with equipment specified in 9.A.Note:Equipment specified in 9.B.1. includes the following:a.For laser gyro equipment, the following equipment used to characterise mirrors, having the threshold accuracy shown or better:1.Scatterometer (10 ppm);2.Reflectometer (50 ppm);3.Profilometer (5 Angstroms);b.For other inertial equipment:1.Inertial Measurement Unit (IMU) Module Tester;2.IMU Platform Tester;3.IMU Stable Element Handling Fixture;4.IMU Platform Balance Fixture;5.Gyro Tuning Test Station;6.Gyro Dynamic Balance Station;7.Gyro Run-In/Motor Test Station;8.Gyro Evacuation and Filling Station;9.Centrifuge Fixture for Gyro Bearings;10.Accelerometer Axis Align Station;11.Accelerometer Test Station;12.Fibre Optic Gyro Coil Winding Machines.

7DSoftware

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
7D002	"Source code" for the operation or maintenance of any inertial navigation equipment, including inertial equipment not specified in 7A003 or 7A004, or Attitude and Heading Reference Systems ("AHRS").Note:7D002 does not control "source code" for the "use" of gimballed "AHRS".Technical Note:"AHRS" generally differ from Inertial Navigation Systems (INS) in that an "AHRS" provides attitude and heading information and normally does not provide the acceleration, velocity and position information associated with an INS.	M2D3	"Software", specially designed or modified for the operation or maintenance of "guidance sets" specified in 2.A.1.d.Note:2.D.3. includes "software", specially designed or modified to enhance the performance of "guidance sets" to achieve or exceed the accuracy specified in 2.A.1.d.
		M9D1	"Software" specially designed or modified for the "use" of equipment specified in 9.A. or 9.B.
7D101	"Software" specially designed or modified for the "use" of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103.	M2D	"Software" specially designed or modified for the "use" of "production facilities" specified in 2.B.1.
		M9D1	"Software" specially designed or modified for the "use" of equipment specified in 9.A. or 9.B.
		M10D1	"Software" specially designed or modified for the "use" of equipment specified in 10.A. or 10.B.Note:"Software" specified in 10.D.1. may be exported as part of a manned aircraft or satellite or in quantities appropriate for replacement parts for manned aircraft.
		M11D1&2	"Software" specially designed or modified for the "use" of equipment specified in 11.A.1., 11.A.2. or 11.A.4."Software" specially designed for the "use" of equipment specified in 11.A.3.
7D102	Integration "software" as follows:a.Integration "software" for the equipment specified in 7A103.b.;	M9D2	Integration "software" for the equipment specified in 9.A.1.
	b.Integration "software" specially designed for the equipment specified in 7A003 or 7A103.a.	M9D3*	Integration "software" specially designed for the equipment specified in 9.A.6.
	c.Integration "software" designed or modified for the equipment specified in 7A103.c.Note:A common form of integration "software" employs Kalman filtering.	M9D4	Integration "software", designed or modified for the "integrated navigation systems" specified in 9.A.7.Note:A common form of integration "software" employs Kalman filtering.
7D103	"Software" specially designed for modelling or simulation of the "guidance sets" specified in 7A117 or for their design integration with the space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.Note:"Software" specified in 7D103 remains controlled when combined with specially designed hardware specified in 4A102.	M16D1	"Software" specially designed for modelling, simulation, or design integration of the systems specified in 1.A. or the subsystems specified in 2.A or 20.A.Technical Note:The modelling includes in particular the aerodynamic and thermodynamic analysis of the systems.

7ETechnology

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
7E001	"Technology" according to the General Technology Note for the "development" of equipment or "software", specified in 7A, 7B, 7D001, 7D002, 7D003, 7D005 and 7D101 to 7D103.Note:7E001 includes key management "technology" exclusively for equipment specified in 7A005.a.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
7E002	"Technology" according to the General Technology Note for the "production" of equipment specified in 7A or 7B.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
7E003	"Technology" according to the General Technology Note for the repair, refurbishing or overhaul of equipment specified in 7A001 to 7A004.Note:7E003 does not control maintenance "technology" directly associated with calibration, removal or replacement of damaged or unserviceable LRUs and SRAs of a "civil aircraft" as described in "Maintenance Level I" or "Maintenance Level II".N.B.:See Technical Notes to 7B001.	M2E1	"Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 2.A., 2.B. or 2.D.
		M9E1	"Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 9.A., 9.B. or 9.D.Note:Equipment or "software" specified in 9.A. or 9.D. may be exported as part of a manned aircraft, satellite, land vehicle, marine/submarine vessel or geophysical survey equipment or in quantities appropriate for replacement parts for such applications.
7E004	Other "technology" as follows:a."Technology" for the "development" or "production" of any of the following:1.Not used;2.Air data systems based on surface static data only, i.e., which dispense with conventional air data probes;3.Three dimensional displays for "aircraft";4.Not used;5.Electric actuators (i.e., electromechanical, electrohydrostatic and integrated actuator package) specially designed for "primary flight control";6."Flight control optical sensor array" specially designed for implementing "active flight control systems"; or7."DBRN" systems designed to navigate underwater, using sonar or gravity databases, that provide a positioning accuracy equal to or less (better) than 0,4 nautical miles;b."Development" "technology", as follows, for "active flight control systems" (including "fly-by-wire systems" or "fly-by-light systems"):1.Photonic-based "technology" for sensing aircraft or flight control component state, transferring flight control data, or commanding actuator movement, "required" for "fly-by-light systems" "active flight control systems";2.Not used;3.Real-time algorithms to analyze component sensor information to predict and preemptively mitigate impending degradation and failures of components within an "active flight control system";Note:7E004.b.3. does not control algorithms for purpose of off-line maintenance.4.Real-time algorithms to identify component failures and reconfigure force and moment controls to mitigate "active flight control system" degradations and failures;Note:7E004.b.4. does not control algorithms for the elimination of fault effects through comparison of redundant data sources, or off-line pre-planned responses to anticipated failures.5.Integration of digital flight control, navigation and propulsion control data, into a digital flight management system for "total control of flight";
	Note:7E004.b.5. does not control:a."Development" "technology" for integration of digital flight control, navigation and propulsion control data, into a digital flight management system for "flight path optimisation";b."Development" "technology" for "aircraft" flight instrument systems integrated solely for VOR, DME, ILS or MLS navigation or approaches.6.Not used;7."Technology" "required" for deriving the functional requirements for "fly-by-wire systems" having all of the following:a."Inner-loop" airframe stability controls requiring loop closure rates of 40 Hz or greater; andTechnical Note:"Inner-loop" refers to functions of "active flight control systems" that automate airframe stability controls.b.Having any of the following:1.Corrects an aerodynamically unstable airframe, measured at any point in the design flight envelope, that would lose recoverable control if not corrected within 0,5 seconds;2.Couples controls in two or more axes while compensating for "abnormal changes in aircraft state";Technical Note:"Abnormal changes in aircraft state" include in-flight structural damage, loss of engine thrust, disabled control surface, or destabilizing shifts in cargo load.3.Preforms the functions specified in 7E004.b.5.; orNote:7E004.b.7.b.3. does not control autopilots.4.Enables aircraft to have stable controlled flight, other than during take-off or landing, at greater than 18 degrees angle of attack, 15 degrees side slip, 15 degrees/second pitch or yaw rate, or 90 degrees/second roll rate;8."Technology" "required" for deriving the functional requirements for "fly-by-wire systems" to achieve all of the following:a.No loss of control of the aircraft in the event of a consecutive sequence of any two individual faults within the "fly-by-wire system"; andb.Probability of loss of control of the aircraft being less (better) than 1 × 10–9 failures per flight hour;Note:7E004.b. does not control technology associated with common computer elements and utilities (e.g., input signal acquisition, output signal transmission, computer program and data loading, built-in test, task scheduling mechanisms) not providing a specific flight control system function.c."Technology" for the "development" of helicopter systems, as follows:1.Multi-axis fly-by-wire or fly-by-light controllers, which combine the functions of at least two of the following into one controlling element:a.Collective controls;b.Cyclic controls;c.Yaw controls;2."Circulation-controlled anti-torque or circulation-controlled directional control systems";3.Rotor blades incorporating "variable geometry airfoils", for use in systems using individual blade control.	M10E1	Design "technology" for integration of air vehicle fuselage, propulsion system and lifting control surfaces, designed or modified for the systems specified in 1.A. or 19.A.2., to optimise aerodynamic performance throughout the flight regime of an unmanned aerial vehicle.
7E101	"Technology" according to the General Technology Note for the "use" of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115 to 7A117, 7B001, 7B002, 7B003, 7B102, 7B103, 7D101 to 7D103.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
7E102	"Technology" for protection of avionics and electrical subsystems against electromagnetic pulse (EMP) and electromagnetic interference (EMI) hazards, from external sources, as follows:a.Design "technology" for shielding systems;b.Design "technology" for the configuration of hardened electrical circuits and subsystems;c.Design "technology" for the determination of hardening criteria of 7E102.a. and 7E102.b.	M11E1	Design "technology" for protection of avionics and electrical subsystems against Electromagnetic Pulse (EMP) and Electromagnetic Interference (EMI) hazards from external sources, as follows:a.Design "technology" for shielding systems;b.Design "technology" for the configuration of hardened electrical circuits and subsystems;c.Design "technology" for determination of hardening criteria for the above.
7E104	"Technology" for the integration of the flight control, guidance, and propulsion data into a flight management system for optimization of rocket system trajectory.	M10E2	Design "technology" for integration of the flight control, guidance, and propulsion data into a flight management system, designed or modified for the systems specified in 1.A. or 19.A.1., for optimisation of rocket system trajectory.

CATEGORY 9 — AEROSPACE AND PROPULSION9ASystems, Equipment and Components

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
9A001	Aero gas turbine engines having any of the following:N.B.:SEE ALSO 9A101.a.Incorporating any of the "technologies" specified in 9E003.a., 9E003.h. or 9E003.i.; orNote 1:9A001.a. does not control aero gas turbine engines which meet all of the following:a.Certified by the civil aviation authorities of one or more "participating states"; andb.Intended to power non-military manned aircraft for which any of the following has been issued by civil aviation authorities of one or more "participating states" for the aircraft with this specific engine type:1.A civil type certificate; or2.An equivalent document recognized by the International Civil Aviation Organisation (ICAO).Note 2:9A001.a. does not control aero gas turbine engines designed for Auxiliary Power Units (APUs) approved by the civil aviation authority in a "participating state".b.Designed to power an aircraft to cruise at Mach 1 or higher, for more than thirty minutes.	M3A1	Turbojet and turbofan engines, as follows:a.Engines having both of the following characteristics:1."Maximum thrust value" greater than 400 N (achieved un-installed) excluding civil certified engines with a "maximum thrust value" greater than 8,89 kN (achieved un-installed); and2.Specific fuel consumption of 0,15 kg N–1 h–1 or less (at maximum continuous power at sea level static conditions using the ICAO standard atmosphere);Technical Note:In 3.A.1.a.1., "maximum thrust value" is the manufacturer's demonstrated maximum thrust for the engine type un-installed. The civil type certified thrust value will be equal to or less than the manufacturer's demonstrated maximum thrust for the engine type.b.Engines designed or modified for systems specified in 1.A. or 19.A.2., regardless of thrust or specific fuel consumption.Note:Engines specified in 3.A.1. may be exported as part of a manned aircraft or in quantities appropriate for replacement parts for a manned aircraft.
9A004	Space launch vehicles, "spacecraft", "spacecraft buses", "spacecraft payloads", "spacecraft" on-board systems or equipment, and terrestrial equipment, as follows:N.B.:SEE ALSO 9A104.a.Space launch vehicles;b."Spacecraft";c."Spacecraft buses";d."Spacecraft payloads" incorporating items specified in 3A001.b.1.a.4., 3A002.g., 5A001.a.1., 5A001.b.3., 5A002.a.5., 5A002.a.9., 6A002.a.1., 6A002.a.2., 6A002.b., 6A002.d., 6A003.b., 6A004.c., 6A004.e., 6A008.d., 6A008.e., 6A008.k., 6A008.l. or 9A010.c.;e.On-board systems or equipment, specially designed for "spacecraft" and having any of the following functions:1."Command and telemetry data handling";Note:For the purpose of 9A004.e.1., "command and telemetry data handling" includes bus data management, storage, and processing.2."Payload data handling"; orNote:For the purpose of 9A004.e.2., "payload data handling" includes payload data management, storage, and processing.3."Attitude and orbit control";Note:For the purpose of 9A004.e.3., "attitude and orbit control" includes sensing and actuation to determine and control the position and orientation of a "spacecraft".N.B.:For equipment specially designed for military use, see Military Goods Controls.f.Terrestrial equipment, specially designed for "spacecraft" as follows:1.Telemetry and telecommand equipment;2.Simulators.	M1A1	Complete rocket systems (including ballistic missile systems, space launch vehicles, and sounding rockets) capable of delivering at least a 500 kg "payload" to a "range" of at least 300 km.
		M19A1	Complete rocket systems (including ballistic missile systems, space launch vehicles, and sounding rockets), not specified in 1.A.1., capable of a "range" equal to or greater than 300 km.
9A005	Liquid rocket propulsion systems containing any of the systems or components, specified in 9A006.N.B.:SEE ALSO 9A105 AND 9A119.	M2A1a	Individual rocket stages usable in the systems specified in 1.A.;
		M2A1c	Rocket propulsion subsystems, usable in the systems specified in 1.A., as follows;1.Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 1,1 × 106 Ns;2.Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 1,1 × 106 Ns;Note:Liquid propellant apogee engines or station-keeping engines specified in 2.A.1.c.2., designed or modified for use on satellites, may be treated as Category II, if the subsystem is exported subject to end-use statements and quantity limits appropriate for the excepted end-use stated above, when having a vacuum thrust not greater than 1kN.
		M20A1	Complete subsystems as follows:a.Individual rocket stages, not specified in 2.A.1., usable in systems specified in 19.A.;b.Rocket propulsion subsystems, not specified in 2.A.1., usable in the systems specified in 19.A.1., as follows:1.Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 8,41 × 105 Ns, but less than 1,1 × 106 Ns;2.Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 8,41 × 105 Ns, but less than 1,1 × 106 Ns;
9A006	Systems and components, specially designed for liquid rocket propulsion systems, as follows:N.B.:SEE ALSO 9A106, 9A108 AND 9A120.a.Cryogenic refrigerators, flightweight dewars, cryogenic heat pipes or cryogenic systems, specially designed for use in space vehicles and capable of restricting cryogenic fluid losses to less than 30 % per year;
	b.Cryogenic containers or closed-cycle refrigeration systems, capable of providing temperatures of 100 K (–173 °C) or less for "aircraft" capable of sustained flight at speeds exceeding Mach 3, launch vehicles or "spacecraft";c.Slush hydrogen storage or transfer systems;d.High pressure (exceeding 17,5 MPa) turbo pumps, pump components or their associated gas generator or expander cycle turbine drive systems;	M3A8	Liquid propellant tanks specially designed for the propellants controlled in Item 4.C. or other liquid propellants used in the systems specified in 1.A.1.
		M3A5	Liquid, slurry and gel propellant (including oxidisers) control systems, and specially designed components therefor, usable in the systems specified in 1.A., designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz.Notes:1.The only servo valves, pumps and gas turbines specified in 3.A.5. are the following:a.Servo valves designed for flow rates equal to or greater than 24 litres per minute, at an absolute pressure equal to or greater than 7 MPa, that have an actuator response time of less than 100 ms.b.Pumps, for liquid propellants, with shaft speeds equal to or greater than 8000 rpm at the maximum operating mode or with discharge pressures equal to or greater than 7 MPa.c.Gas turbines, for liquid propellant turbopumps, with shaft speeds equal to or greater than 8000 rpm at the maximum operating mode.2.Systems and components specified in 3.A.5. may be exported as part of a satellite.
	e.High-pressure (exceeding 10,6 MPa) thrust chambers and nozzles therefor;	M3A10	Combustion chambers and nozzles for liquid propellant rocket engines usable in the subsystems specified in 2.A.1.c.2. or 20.A.1.b.2.
	f.Propellant storage systems using the principle of capillary containment or positive expulsion (i.e., with flexible bladders);	M3A8
	g.Liquid propellant injectors with individual orifices of 0,381 mm or smaller in diameter (an area of 1,14 × 10–3 cm2 or smaller for non-circular orifices) and specially designed for liquid rocket engines;	M3A5
	h.One-piece carbon-carbon thrust chambers or one-piece carbon-carbon exit cones, with densities exceeding 1,4 g/cm3 and tensile strengths exceeding 48 MPa.	M3A10
9A007	Solid rocket propulsion systems having any of the following:N.B.:SEE ALSO 9A107 AND 9A119.a.Total impulse capacity exceeding 1,1 MNs;b.Specific impulse of 2,4 kNs/kg or more, when the nozzle flow is expanded to ambient sea level conditions for an adjusted chamber pressure of 7 MPa;c.Stage mass fractions exceeding 88 % and propellant solid loadings exceeding 86 %;d.Components specified in 9A008; ore.Insulation and propellant bonding systems, using direct-bonded motor designs to provide a "strong mechanical bond" or a barrier to chemical migration between the solid propellant and case insulation material.Technical Note:"Strong mechanical bond" means bond strength equal to or more than propellant strength.	M2A1	Complete subsystems usable in the systems specified in 1.A., as follows:a.Individual rocket stages usable in the systems specified in 1.A.;b.Re-entry vehicles, and equipment designed or modified therefor, usable in the systems specified in 1.A., as follows, except as provided in the Note below 2.A.1. for those designed for non-weapon payloads:1.Heat shields, and components therefor, fabricated of ceramic or ablative materials;2.Heat sinks and components therefor, fabricated of light-weight, high heat capacity materials;3.Electronic equipment specially designed for re-entry vehicles;c.Rocket propulsion subsystems, usable in the systems specified in 1.A., as follows;1.Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 1,1 × 106 Ns;2.Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 1,1 × 106 Ns;Note:Liquid propellant apogee engines or station-keeping engines specified in 2.A.1.c.2., designed or modified for use on satellites, may be treated as Category II, if the subsystem is exported subject to end-use statements and quantity limits appropriate for the excepted end-use stated above, when having a vacuum thrust not greater than 1kN.d."Guidance sets", usable in the systems specified in 1.A., capable of achieving system accuracy of 3,33 % or less of the "range" (e.g. a "CEP" of 10 km or less at a "range" of 300 km), except as provided in the Note below 2.A.1. for those designed for missiles with a "range" under 300 km or manned aircraft;Technical Notes:1.A "guidance set" integrates the process of measuring and computing a vehicle's position and velocity (i.e. navigation) with that of computing and sending commands to the vehicle's flight control systems to correct the trajectory.2."CEP" (circle of equal probability) is a measure of accuracy, defined as the radius of the circle centred at the target, at a specific range, in which 50 % of the payloads impact.e.Thrust vector control subsystems, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for rocket systems that do not exceed the "range"/"payload" capability of systems specified in 1.A.;Technical Note:2.A.1.e. includes the following methods of achieving thrust vector control:a.Flexible nozzle;b.Fluid or secondary gas injection;c.Movable engine or nozzle;d.Deflection of exhaust gas stream (jet vanes or probes);e.Use of thrust tabs.f.Weapon or warhead safing, arming, fuzing, and firing mechanisms, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for systems other than those specified in 1.A.Note:The exceptions in 2.A.1.b., 2.A.1.d., 2.A.1.e. and 2.A.1.f. above may be treated as Category II if the subsystem is exported subject to end-use statements and quantity limits appropriate for the excepted end-use stated above.Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 1,1 × 106 Ns;
		M2A1c1
9A008	Components specially designed for solid rocket propulsion systems, as follows:N.B.:SEE ALSO 9A108.a.Insulation and propellant bonding systems, using liners to provide a "strong mechanical bond" or a barrier to chemical migration between the solid propellant and case insulation material;Technical Note:"Strong mechanical bond" means bond strength equal to or more than propellant strength.	M3A3	Rocket motor cases, "insulation" components and nozzles therefor, usable in the systems specified in 1.A. or 19.A.1.Technical Note:In 3.A.3. "insulation" intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber components comprising sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps.Note:Refer to 3.C.2. for "insulation" material in bulk or sheet form.
		M3C1	"Interior lining" usable for rocket motor cases in the subsystems specified in 2.A.1.c.1. or specially designed for subsystems specified in 20.A.1.b.1.Technical Note:In 3.C.1. "interior lining" suited for the bond interface between the solid propellant and the case or insulating liner is usually a liquid polymer based dispersion of refractory or insulating materials e.g. carbon filled HTPB or other polymer with added curing agents to be sprayed or screeded over a case interior.
	b.Filament-wound "composite" motor cases exceeding 0,61 m in diameter or having "structural efficiency ratios (PV/W)" exceeding 25 km;Technical Note:"Structural efficiency ratio (PV/W)" is the burst pressure (P) multiplied by the vessel volume (V) divided by the total pressure vessel weight (W).	M3C2	"Insulation" material in bulk form usable for rocket motor cases in the subsystems specified in 2.A.1.c.1. or specially designed for subsystems specified in 20.A.1.b.1.Technical Note:In 3.C.2. "insulation" intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps specified in 3.A.3.
	c.Nozzles with thrust levels exceeding 45 kN or nozzle throat erosion rates of less than 0,075 mm/s;d.Movable nozzle or secondary fluid injection thrust vector control systems, capable of any of the following:1.Omni-axial movement exceeding ± 5°;2.Angular vector rotations of 20°/s or more; or3.Angular vector accelerations of 40°/s2 or more	M2A1e	Thrust vector control subsystems, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for rocket systems that do not exceed the "range"/"payload" capability of systems specified in 1.A.;Technical Note:2.A.1.e. includes the following methods of achieving thrust vector control:a.Flexible nozzle;b.Fluid or secondary gas injection;c.Movable engine or nozzle;d.Deflection of exhaust gas stream (jet vanes or probes);e.Use of thrust tabs.
9A009	Hybrid rocket propulsion systems having any of the following:N.B.:SEE ALSO 9A109 AND 9A119.a.Total impulse capacity exceeding 1,1 MNs; orb.Thrust levels exceeding 220 kN in vacuum exit conditions.	M2A1c1	Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 1,1 × 106 Ns;
		M20A1b	Rocket propulsion subsystems, not specified in 2.A.1., usable in the systems specified in 19.A.1., as follows:1.Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 8,41 × 105 Ns, but less than 1,1 × 106 Ns;2.Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 8,41 × 105 Ns, but less than 1,1 × 106 Ns;
9A010	Specially designed components, systems and structures, for launch vehicles, launch vehicle propulsion systems or "spacecraft", as follows:N.B.:SEE ALSO 1A002 AND 9A110.a.Components and structures, each exceeding 10 kg and specially designed for launch vehicles manufactured using any of the following:1."Composite" materials consisting of "fibrous or filamentary materials" specified in 1C0010.e. and resins specified in 1C008 or 1C009.b.;2.Metal "matrix" "composites" reinforced by any of the following:a.Materials specified in 1C007;b."Fibrous or filamentary materials" specified in 1C010; orc.Aluminides specified in 1C002.a.; or3.Ceramic "matrix" "composite" materials specified in 1C007;Note:The weight cut-off is not relevant for nose cones.	M6A1	Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A.
	b.Components and structures, specially designed for launch vehicle propulsion systems specified in 9A005 to 9A009 manufactured using any of the following:1."Fibrous or filamentary materials" specified in 1C010.e. and resins specified in 1C008 or 1C009.b.;2.Metal "matrix" "composites" reinforced by any of the following:a.Materials specified in 1C007;b."Fibrous or filamentary materials" specified in 1C010; orc.Aluminides specified by 1C002.a.; or3.Ceramic "matrix" "composite" materials specified in 1C007;	M6A1	Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A.
	c.Structural components and isolation systems, specially designed to control actively the dynamic response or distortion of "spacecraft" structures;	M6A1	Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A.
	d.Pulsed liquid rocket engines with thrust-to-weight ratios equal to or more than 1 kN/kg and a response time (the time required to achieve 90 % of total rated thrust from start-up) of less than 30 ms.	M3A2	Ramjet/scramjet/pulse jet/"combined cycle engines", including devices to regulate combustion, and specially designed components therefor, usable in the systems specified in 1.A. or 19.A.2.Technical Note:In Item 3.A.2., "combined cycle engines" are the engines that employ two or more cycles of the following types of engines: gas-turbine engine (turbojet, turboprop, turbofan and turboshaft), ramjet, scramjet, pulse jet, pulse detonation engine, rocket motor (liquid/solid-propellant and hybrid).
9A011	Ramjet, scramjet or combined cycle engines, and specially designed components therefor.N.B.:SEE ALSO 9A111 AND 9A118.	M3A2	Ramjet/scramjet/pulse jet/"combined cycle engines", including devices to regulate combustion, and specially designed components therefor, usable in the systems specified in 1.A. or 19.A.2.Technical Note:In Item 3.A.2., "combined cycle engines" are the engines that employ two or more cycles of the following types of engines: gas-turbine engine (turbojet, turboprop, turbofan and turboshaft), ramjet, scramjet, pulse jet, pulse detonation engine, rocket motor (liquid/solid-propellant and hybrid).
9A012	"Unmanned aerial vehicles" ("UAVs"), unmanned "airships", related equipment and components, as follows:N.B.:SEE ALSO 9A112.a."UAVs" or unmanned "airships", designed to have controlled flight out of the direct "natural vision" of the "operator" and having any of the following:1.Having all of the following:a.A maximum "endurance" greater than or equal to 30 minutes but less than 1 hour; andb.Designed to take-off and have stable controlled flight in wind gusts equal to or exceeding 46,3 km/h (25 knots); or2.A maximum "endurance" of 1 hour or greater;Technical Notes:1.For the purposes of 9A012.a., "operator" is a person who initiates or commands the "UAV" or unmanned "airship" flight.2.For the purposes of 9A012.a., "endurance" is to be calculated for ISA conditions (ISO 2533:1975) at sea level in zero wind.3.For the purposes of 9A012.a., "natural vision" means unaided human sight, with or without corrective lenses.b.Related equipment and components, as follows:1.Not used2.Not used	M1A2	Complete unmanned aerial vehicle systems (including cruise missile systems, target drones and reconnaissance drones) capable of delivering at least a 500 kg "payload" to a "range" of at least 300 km.
		M19A	ITEM 19 OTHER COMPLETE DELIVERY SYSTEMS: equipment, assemblies and components
	3.Equipment or components, specially designed to convert a manned "aircraft" or manned "airship", to a "UAV" or unmanned "airship", specified in 9A012.a.;4.Air breathing reciprocating or rotary internal combustion type engines, specially designed or modified to propel "UAVs" or unmanned "airships", at altitudes above 15240 metres (50000 feet).	M9A6	Inertial or other equipment using accelerometers specified in 9.A.3. or 9.A.5. or gyros specified in 9.A.4. or 9.A.5., and systems incorporating such equipment, and specially designed components therefor.
9A101	Turbojet and turbofan engines, other than those specified in 9A001, as follows;a.Engines having both of the following characteristics:1."Maximum thrust value" greater than 400 N (achieved un-installed) excluding civil certified engines with a "maximum thrust value" greater than 8890 N (achieved un-installed), and2.Specific fuel consumption of 0,15 kg/N/hr or less (at maximum continuous power at sea level static conditions using the ICAO standard atmosphere);Technical Note:For the purpose of 9A101.a.1. "maximum thrust value" is the manufacturer's demonstrated maximum thrust for the engine type un-installed. The civil type certified thrust value will be equal or less than the manufacturer's demonstrated maximum thrust for the engine type.b.Engines designed or modified for use in "missiles" or unmanned aerial vehicles specified in 9A012 or 9A112.a.,	M3A1	Turbojet and turbofan engines, as follows:a.Engines having both of the following characteristics:1."Maximum thrust value" greater than 400 N (achieved un-installed) excluding civil certified engines with a "maximum thrust value" greater than 8,89 kN (achieved un-installed); and2.Specific fuel consumption of 0,15 kg N–1 h–1 or less (at maximum continuous power at sea level static conditions using the ICAO standard atmosphere);Technical Note:In 3.A.1.a.1., "maximum thrust value" is the manufacturer's demonstrated maximum thrust for the engine type un-installed. The civil type certified thrust value will be equal to or less than the manufacturer's demonstrated maximum thrust for the engine type.b.Engines designed or modified for systems specified in 1.A. or 19.A.2., regardless of thrust or specific fuel consumption.Note:Engines specified in 3.A.1. may be exported as part of a manned aircraft or in quantities appropriate for replacement parts for a manned aircraft.
9A102	"Turboprop engine systems" specially designed for unmanned aerial vehicles specified in 9A012 or 9A112.a., and specially designed components therefor, having a "maximum power" greater than 10 kW.Note:9A102 does not control civil certified engines.Technical Notes:1.For the purposes of 9A102 a "turboprop engine system" incorporates all of the following:a.Turboshaft engine; andb.Power transmission system to transfer the power to a propeller.2.For the purposes of 9A102 the "maximum power" is achieved uninstalled at sea level static conditions using ICAO standard atmosphere.	M3A9	"Turboprop engine systems" specially designed for the systems in 1.A.2. or 19.A.2., and specially designed components therefor, having a maximum power greater than 10 kW (achieved uninstalled at sea level static conditions using the ICAO standard atmosphere), excluding civil certified engines.Technical Note:For the purposes of Item 3.A.9., a "turboprop engine system" incorporates all of the following: a. Turboshaft engine; and b. Power transmission system to transfer the power to a propeller.
9A104	Sounding rockets, capable of a range of at least 300 km.N.B.:SEE ALSO 9A004.	M1A1	Complete rocket systems (including ballistic missile systems, space launch vehicles, and sounding rockets) capable of delivering at least a 500 kg "payload" to a "range" of at least 300 km.
		M19A1	Complete rocket systems (including ballistic missile systems, space launch vehicles, and sounding rockets), not specified in 1.A.1., capable of a "range" equal to or greater than 300 km.
9A105	Liquid propellant rocket engines, as follows:N.B.:SEE ALSO 9A119.
	a.Liquid propellant rocket engines usable in "missiles", other than those specified in 9A005, integrated, or designed or modified to be integrated, into a liquid propellant propulsion system which has a total impulse capacity equal to or greater than 1,1 MNs;	M2A1c2	Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 1,1 × 106 Ns;
	b.Liquid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005 or 9A105.a., integrated, or designed or modified to be integrated, into a liquid propellant propulsion system which has a total impulse capacity equal to or greater than 0,841 MNs	M20A1b2	Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 8,41 × 105 Ns, but less than 1,1 × 106 Ns
9A106	Systems or components, other than those specified in 9A006 as follows, specially designed for liquid rocket propulsion systems:a.Ablative liners for thrust or combustion chambers, usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;b.Rocket nozzles, usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;	M3A3	Rocket motor cases, "insulation" components and nozzles therefor, usable in the systems specified in 1.A. or 19.A.1.Technical Note:In 3.A.3. "insulation" intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber components comprising sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps.Note:Refer to 3.C.2. for "insulation" material in bulk or sheet form.
	c.Thrust vector control sub-systems, usable in "missiles";Technical Note:Examples of methods of achieving thrust vector control specified in 9A106.c. are:1.Flexible nozzle;2.Fluid or secondary gas injection;3.Movable engine or nozzle;4.Deflection of exhaust gas stream (jet vanes or probes); or5.Thrust tabs.	M2A1e	Thrust vector control subsystems, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for rocket systems that do not exceed the "range"/"payload" capability of systems specified in 1.A.; TechnicalTechnical Note:2.A.1.e. includes the following methods of achieving thrust vector control:a.Flexible nozzle;b.Fluid or secondary gas injection;c.Movable engine or nozzle;d.Deflection of exhaust gas stream (jet vanes or probes);e.Use of thrust tabs.
	d.Liquid, slurry and gel propellant (including oxidisers) control systems, and specially designed components therefor, usable in "missiles", designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz;Note:The only servo valves, pumps and gas turbines specified in 9A106.d., are the following:a.Servo valves designed for flow rates equal to or greater than 24 litres per minute, at an absolute pressure equal to or greater than 7 MPa, that have an actuator response time of less than 100 ms;b.Pumps, for liquid propellants, with shaft speeds equal to or greater than 8000 r.p.m. at a maximum operating mode or with discharge pressures equal to or greater than 7 MPa.c.Gas turbines, for liquid propellant turbopumps, with shaft speeds equal to or greater than 8000 r.p.m. at the maximum operating mode.	M3A5	Liquid, slurry and gel propellant (including oxidisers) control systems, and specially designed components therefor, usable in the systems specified in 1.A., designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz.Notes:1.The only servo valves, pumps and gas turbines specified in 3.A.5. are the following:a.Servo valves designed for flow rates equal to or greater than 24 litres per minute, at an absolute pressure equal to or greater than 7 MPa, that have an actuator response time of less than 100 ms.b.Pumps, for liquid propellants, with shaft speeds equal to or greater than 8000 rpm at the maximum operating mode or with discharge pressures equal to or greater than 7 MPa.c.Gas turbines, for liquid propellant turbopumps, with shaft speeds equal to or greater than 8000 rpm at the maximum operating mode.2.Systems and components specified in 3.A.5. may be exported as part of a satellite.
	e.Combustion chambers and nozzles, usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.	M3A10	Combustion chambers and nozzles for liquid propellant rocket engines usable in the subsystems specified in 2.A.1.c.2. or 20.A.1.b.2.
9A107	Solid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A007, having total impulse capacity equal to or greater than 0,841 MNs.N.B.:SEE ALSO 9A119.	M20A1b1	Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 8,41 × 105 Ns, but less than 1,1 × 106 Ns;
9A108	Components, other than those specified in 9A008, as follows, specially designed for solid rocket propulsion systems:a.Rocket motor cases and "insulation" components therefor, usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;b.Rocket nozzles, usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;	M3A3	Rocket motor cases, "insulation" components and nozzles therefor, usable in the systems specified in 1.A. or 19.A.1.
		M3A3	Technical Note:In 3.A.3. "insulation" intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber components comprising sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps.Note:Refer to 3.C.2. for "insulation" material in bulk or sheet form.
	c.Thrust vector control sub-systems, usable in "missiles".Technical Note:Examples of methods of achieving thrust vector control specified in 9A108.c. are:1.Flexible nozzle;2.Fluid or secondary gas injection;3.Movable engine or nozzle;4.Deflection of exhaust gas stream (jet vanes or probes); or5.Thrust tabs.	M2A1e	Thrust vector control subsystems, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for rocket systems that do not exceed the "range"/"payload" capability of systems specified in 1.A.;Technical Note:2.A.1.e. includes the following methods of achieving thrust vector control:a.Flexible nozzle;b.Fluid or secondary gas injection;c.Movable engine or nozzle;d.Deflection of exhaust gas stream (jet vanes or probes);e.Use of thrust tabs.
9A109	Hybrid rocket motors and specially designed components as follows:a.Hybrid rocket motors usable in complete rocket systems or unmanned aerial vehicles, capable of 300 km, other than those specified in 9A009, having a total impulse capacity equal to or greater than 0,841 MNs, and specially designed components therefor;b.Specially designed components for hybrid rocket motors specified in 9A009 that are usable in "missiles".N.B.:SEE ALSO 9A009 and 9A119.	M3A6	Specially designed components for hybrid rocket motors specified in 2.A.1.c.1. and 20.A.1.b.1.
		M20A1b	Rocket propulsion subsystems, not specified in 2.A.1., usable in the systems specified in 19.A.1., as follows:1.Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 8,41 × 105 Ns, but less than 1,1 × 106 Ns;2.Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 8,41 × 105 Ns, but less than 1,1 × 106 Ns;
		M2A1c	Rocket propulsion subsystems, usable in the systems specified in 1.A., as follows;1.Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 1,1 × 106 Ns;2.Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 1,1 × 106 Ns;Note:Liquid propellant apogee engines or station-keeping engines specified in 2.A.1.c.2., designed or modified for use on satellites, may be treated as Category II, if the subsystem is exported subject to end-use statements and quantity limits appropriate for the excepted end-use stated above, when having a vacuum thrust not greater than 1kN.
9A110	Composite structures, laminates and manufactures thereof, other than those specified in 9A010, specially designed for use in "missiles" or the subsystems specified in 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119.N.B.:SEE ALSO 1A002.Technical Note:In 9A110 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M6A1	Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A.
9A111	Pulse jet engines, usable in "missiles" or unmanned aerial vehicles specified in 9A012 or 9A112.a., and specially designed components therefor.N.B.:SEE ALSO 9A011 AND 9A118.	M3A2	Ramjet/scramjet/pulse jet/"combined cycle engines", including devices to regulate combustion, and specially designed components therefor, usable in the systems specified in 1.A. or 19.A.2.Technical Note:In Item 3.A.2., "combined cycle engines" are the engines that employ two or more cycles of the following types of engines: gas-turbine engine (turbojet, turboprop, turbofan and turboshaft), ramjet, scramjet, pulse jet, pulse detonation engine, rocket motor (liquid/solid-propellant and hybrid)
9A112	"Unmanned aerial vehicles" ("UAVs"), other than those specified in 9A012, as follows:a."Unmanned aerial vehicles" ("UAVs") capable of a range of 300 km;b."Unmanned aerial vehicles" ("UAVs") having all of the following:1.Having any of the following:a.An autonomous flight control and navigation capability; orb.Capability of controlled flight out of the direct vision range involving a human operator; and2.Having any of the following:a.Incorporating an aerosol dispensing system/mechanism with a capacity greater than 20 litres; orb.Designed or modified to incorporate an aerosol dispensing system/mechanism with a capacity greater than 20 litres.Technical Notes:1.An aerosol consists of particulate or liquids other than fuel components, by products or additives, as part of the "payload" to be dispersed in the atmosphere. Examples of aerosols include pesticides for crop dusting and dry chemicals for cloud seeding.2.An aerosol dispensing system/mechanism contains all those devices (mechanical, electrical, hydraulic, etc.), which are necessary for storage and dispersion of an aerosol into the atmosphere. This includes the possibility of aerosol injection into the combustion exhaust vapour and into the propeller slip stream.	M19A2	Complete unmanned aerial vehicle systems (including cruise missile systems, target drones and reconnaissance drones), not specified in 1.A.2., capable of a "range" equal to or greater than 300 km.
		M19A3	Complete unmanned aerial vehicle systems, not specified in 1.A.2. or 19.A.2., having all of the following:a.Having any of the following:1.An autonomous flight control and navigation capability; or2.Capability of controlled flight out of the direct vision range involving a human operator; andb.Having any of the following:1.Incorporating an aerosol dispensing system/mechanism with a capacity greater than 20 litres; or2.Designed or modified to incorporate an aerosol dispensing system/mechanism with a capacity greater than 20 litres.Note:Item 19.A.3. does not control model aircraft, specially designed for recreational or competition purposes.Technical Notes:1.An aerosol consists of particulate or liquids other than fuel components, by-products or additives, as part of the "payload" to be dispersed in the atmosphere. Examples of aerosols include pesticides for crop dusting and dry chemicals for cloud seeding.
9A115	Launch support equipment as follows:a.Apparatus and devices for handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004, sounding rockets specified in 9A104 or unmanned aerial vehicles specified in 9A012 or 9A112.a.;	M12A1	Apparatus and devices, designed or modified for the handling, control, activation and launching of the systems specified in 1.A., 19.A.1., or 19.A.2.
	b.Vehicles for transport, handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.	M12A2	Vehicles designed or modified for the transport, handling, control, activation and launching of the systems specified in 1.A.
9A116	Reentry vehicles, usable in "missiles", and equipment designed or modified therefor, as follows:a.Reentry vehicles;b.Heat shields and components therefor, fabricated of ceramic or ablative materials;c.Heat sinks and components therefor, fabricated of light-weight, high heat capacity materials;d.Electronic equipment specially designed for reentry vehicles.	M2A1b	Re-entry vehicles, and equipment designed or modified therefor, usable in the systems specified in 1.A., as follows, except as provided in the Note below 2.A.1. for those designed for non-weapon payloads:1.Heat shields, and components therefor, fabricated of ceramic or ablative materials;2.Heat sinks and components therefor, fabricated of light-weight, high heat capacity materials;3.Electronic equipment specially designed for re-entry vehicles;
9A117	Staging mechanisms, separation mechanisms, and interstages, usable in "missiles".N.B.:SEE ALSO 9A121.	M3A4	Staging mechanisms, separation mechanisms, and interstages therefor, usable in the systems specified in 1.A.Note:See also Item 11.A.5.Technical Note:Staging and separation mechanisms specified in 3.A.4. may contain some of the following components:Pyrotechnic bolts, nuts and shackles;Ball locks;Circular cutting devices;Flexible linear shaped charges (FLSC).
9A118	Devices to regulate combustion usable in engines, which are usable in "missiles" or unmanned aerial vehicles specified in 9A012 or 9A112.a., specified in 9A011 or 9A111.	M3A2	Ramjet/scramjet/pulse jet/"combined cycle engines", including devices to regulate combustion, and specially designed components therefor, usable in the systems specified in 1.A. or 19.A.2.Technical Note:In Item 3.A.2., "combined cycle engines" are the engines that employ two or more cycles of the following types of engines: gas-turbine engine (turbojet, turboprop, turbofan and turboshaft), ramjet, scramjet, pulse jet, pulse detonation engine, rocket motor (liquid/solid-propellant and hybrid).
9A119	Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109.	M2A1a	Individual rocket stages usable in the systems specified in 1.A.;
		M20A1a	Complete subsystems as follows: a. Individual rocket stages, not specified in 2.A.1., usable in systems specified in 19.A.
9A120	Liquid propellant tanks, other than those specified in 9A006, specially designed for propellants specified in 1C111 or "other liquid propellants", used in rocket systems capable of delivering at least a 500 kg payload to a range of at least 300 km.	M3A8	Liquid propellant tanks specially designed for the propellants controlled in Item 4.C. or other liquid propellants used in the systems specified in 1.A.1.
9A121	Umbilical and interstage electrical connectors specially designed for "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.Technical Note:Interstage connectors referred to in 9A121 also include electrical connectors installed between the "missile", space launch vehicle or sounding rocket and their payload.	M11A5	Umbilical and interstage electrical connectors specially designed for systems specified in 1.A.1. or 19.A.1.Technical Note:Interstage connectors referred to in 11.A.5. also include electrical connectors installed between systems specified in 1.A.1. or 19.A.1. and their "payload".

9BTest, Inspection and Production Equipment

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
9B005	On-line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use with any of the following:N.B.:SEE ALSO 9B105.a.Wind tunnels designed for speeds of Mach 1,2 or more;Note:9B005.a. does not control wind tunnels specially designed for educational purposes and having a "test section size" (measured laterally) of less than 250 mm.Technical Note:"Test section size" means the diameter of the circle, or the side of the square, or the longest side of the rectangle, at the largest test section location.b.Devices for simulating flow-environments at speeds exceeding Mach 5, including hot-shot tunnels, plasma arc tunnels, shock tubes, shock tunnels, gas tunnels and light gas guns; orc.Wind tunnels or devices, other than two-dimensional sections, capable of simulating Reynolds number flows exceeding 25 × 106.	M15B2	"Aerodynamic test facilities" for speeds of Mach 0,9 or more, usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A. or 20.A.Note:Item 15.B.2 does not control wind tunnels for speeds of Mach 3 or less with dimension of the "test cross section size" equal to or less than 250 mm.Technical Notes:1."Aerodynamic test facilities" includes wind tunnels and shock tunnels for the study of airflow over objects.2."Test cross section size" means the diameter of the circle, or the side of the square, or the longest side of the rectangle, or the major axis of the ellipse at the largest "test cross section" location. "Test cross section" is the section perpendicular to the flow direction.
9B006	Acoustic vibration test equipment capable of producing sound pressure levels of 160 dB or more (referenced to 20 μPa) with a rated output of 4 kW or more at a test cell temperature exceeding 1273 K (1000 °C), and specially designed quartz heaters therefor.N.B.:SEE ALSO 9B106.	M15B4b	Environmental chambers capable of simulating all of the following flight conditions:1.Acoustic environments at an overall sound pressure level of 140 dB or greater (referenced to 2 × 10–5 N/m2 ) or with a total rated acoustic power output of 4 kW or greater; and2.Any of the following: a. Altitude equal to or greater than 15 km; or b. Temperature range from below –50 °C to above 125 °C.
9B105	"Aerodynamic test facilities" for speeds of Mach 0,9 or more, usable for "missiles" and their subsystems.N.B.:SEE ALSO 9B005.Note:9B105 does not control wind-tunnels for speeds of Mach 3 or less with dimension of the "test cross section size" equal to or less than 250 mm.Technical Notes:1.In 9B105 "aerodynamic test facilities" includes wind tunnels and shock tunnels for the study of airflow over objects.2.In Note to 9B105, "test cross section size" means the diameter of the circle, or the side of the square, or the longest side of the rectangle, or the major axis of the ellipse at the largest "test cross section" location. "Test cross section" is the section perpendicular to the flow direction.3.In 9B105 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M15B2	"Aerodynamic test facilities" for speeds of Mach 0,9 or more, usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A. or 20.A.Note:Item 15.B.2 does not control wind tunnels for speeds of Mach 3 or less with dimension of the "test cross section size" equal to or less than 250 mm.Technical Notes:1."Aerodynamic test facilities" includes wind tunnels and shock tunnels for the study of airflow over objects.2."Test cross section size" means the diameter of the circle, or the side of the square, or the longest side of the rectangle, or the major axis of the ellipse at the largest "test cross section" location. "Test cross section" is the section perpendicular to the flow direction.
9B106	Environmental chambers and anechoic chambers, as follows:a.Environmental chambers capable of simulating all the following flight conditions:1.Having any of the following:a.Altitude equal to or greater than 15 km; orb.Temperature range from below 223 K (–50 ° C) to above 398 K (+125 °C); and2.Incorporating, or "designed or modified" to incorporate, a shaker unit or other vibration test equipment to produce vibration environments equal to or greater than 10 g rms, measured "bare table", between 20 Hz and 2 kHz while imparting forces equal to or greater than 5 kN;Technical Notes:1.9B106.a.2. describes systems that are capable of generating a vibration environment with a single wave (e.g., a sine wave) and systems capable of generating a broad band random vibration (i.e., power spectrum).2.In 9B106.a.2., "designed or modified" means the environmental chamber provides appropriate interfaces (e.g., sealing devices) to incorporate a shaker unit or other vibration test equipment as specified in 2B116.3.In 9B106.a.2. "bare table" means a flat table, or surface, with no fixture or fittings.b.Environmental chambers capable of simulating the following flight conditions:1.Acoustic environments at an overall sound pressure level of 140 dB or greater (referenced to 20 μPa) or with a total rated acoustic power output of 4 kW or greater; and2.Altitude equal to or greater than 15 km; or3.Temperature range from below 223 K (–50 °C) to above 398 K (+125 °C).	M15B4	Environmental chambers as follows, usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A. or 20.A.:a.Environmental chambers having all of the following characteristics:1.Capable of simulating any of the following flight conditions:a.Altitude equal to or greater than 15 km; orb.Temperature range from below –50 °C to above 125 °C; and2.Incorporating, or designed or modified to incorporate, a shaker unit or other vibration test equipment to produce vibration environments equal to or greater than 10 g rms, measured "bare table", between 20 Hz and 2 kHz while imparting forces equal to or greater than 5 kN;Technical Notes:1.Item 15.B.4.a.2. describes systems that are capable of generating a vibration environment with a single wave (e.g. a sine wave) and systems capable of generating a broad band random vibration (i.e. power spectrum).2.In Item 15.B.4.a.2., designed or modified means the environmental chamber provides appropriate interfaces (e.g. sealing devices) to incorporate a shaker unit or other vibration test equipment as specified in this Item.b.Environmental chambers capable of simulating all of the following flight conditions:1.Acoustic environments at an overall sound pressure level of 140 dB or greater (referenced to 2 × 10–5 N/m2) or with a total rated acoustic power output of 4 kW or greater; and2.Any of the following:a.Altitude equal to or greater than 15 km; orb.Temperature range from below –50 °C to above 125 °C
9B115	Specially designed "production equipment" for the systems, sub-systems and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.	M2B2	"Production equipment" specially designed for the subsystems specified in 2.A.
		M3B2	"Production equipment" specially designed for equipment or materials specified in 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8., 3.A.9., 3.A.10. or 3.C.
		M20B2	"Production equipment" specially designed for the subsystems specified in 20.A.
9B116	Specially designed "production facilities" for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or "missiles".Technical Note:In 9B116 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M1B1	"Production facilities" specially designed for the systems specified in 1.A
		M2B1	"Production facilities" specially designed for the subsystems specified in 2.A.
		M3B1	"Production facilities" specially designed for equipment or materials specified in 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8., 3.A.9., 3.A.10. or 3.C.
		M19B1	"Production facilities" specially designed for the systems specified in 19.A.1 or 19.A.2.
		M20B1	"Production facilities" specially designed for the subsystems specified in 20.A.
9B117	Test benches and test stands for solid or liquid propellant rockets or rocket motors, having either of the following characteristics:a.The capacity to handle more than 68 kN of thrust; orb.Capable of simultaneously measuring the three axial thrust components.	M15B3	Test benches/stands, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A. or 20.A., which have the capacity to handle solid or liquid propellant rockets, motors or engines having a thrust greater than 68 kN, or which are capable of simultaneously measuring the three axial thrust components.

9CMaterials

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
9C108	"Insulation" material in bulk form and "interior lining", other than those specified in 9A008, for rocket motor cases usable in "missiles" or specially designed for "missiles".Technical Note:In 9C108 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M3C1	"Interior lining" usable for rocket motor cases in the subsystems specified in 2.A.1.c.1. or specially designed for subsystems specified in 20.A.1.b.1.Technical Note:In 3.C.1. "interior lining" suited for the bond interface between the solid propellant and the case or insulating liner is usually a liquid polymer based dispersion of refractory or insulating materials e.g. carbon filled HTPB or other polymer with added curing agents to be sprayed or screeded over a case interior.
		M3C2	"Insulation" material in bulk form usable for rocket motor cases in the subsystems specified in 2.A.1.c.1. or specially designed for subsystems specified in 20.A.1.b.1.Technical Note:In 3.C.2. "insulation" intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps specified in 3.A.3.
9C110	Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for composite structures, laminates and manufactures specified in 9A110, made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a "specific tensile strength" greater than 7,62 × 104 m and a "specific modulus" greater than 3,18 × 106 m.N.B.:SEE ALSO 1C010 AND 1C210.Note:The only resin impregnated fibre prepregs specified in entry 9C110 are those using resins with a glass transition temperature (Tg), after cure, exceeding 418 K (145 °C) as determined by ASTM D4065 or equivalent.	M6C1	Resin impregnated fibre prepregs and metal coated fibre preforms, for the goods specified in 6.A.1., made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a specific tensile strength greater than 7,62 × 104 m and a specific modulus greater than 3,18 × 106 m.Note:The only resin impregnated fibre prepregs specified in 6.C.1. are those using resins with a glass transition temperature (Tg), after cure, exceeding 145 °C as determined by ASTM D4065 or national equivalents.Technical Notes:1.In Item 6.C.1. "specific tensile strength" is the ultimate tensile strength in N/m2 divided by the specific weight in N/m3, measured at a temperature of (296 ± 2)K ((23 ± 2)°C) and a relative humidity of (50 ± 5)%.2.In Item 6.C.1. "specific modulus" is the Young's modulus in N/m2 divided by the specific weight in N/m3, measured at a temperature of (296 ± 2)K ((23 ± 2)°C) and a relative humidity of (50 ± 5)%

9DSoftware

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
9D001	"Software" specially designed or modified for the "development" of equipment or "technology", specified in 9A001 to 9A119, 9B or 9E003.	M3D3	"Software" specially designed or modified for the "development" of equipment specified in 3.A.2., 3.A.3. or 3.A.4.
9D002	"Software" specially designed or modified for the "production" of equipment specified in 9A001 to 9A119 or 9B.	M2D2	"Software" specially designed or modified for the "use" of rocket motors or engines specified in 2.A.1.c.
9D004	Other "software" as follows:a.2D or 3D viscous "software", validated with wind tunnel or flight test data required for detailed engine flow modelling;b."Software" for testing aero gas turbine engines, assemblies or components, specially designed to collect, reduce and analyse data in real time and capable of feedback control, including the dynamic adjustment of test articles or test conditions, as the test is in progress;c."Software" specially designed to control directional solidification or single-crystal material growth in equipment specified in 9B001.a. or 9B001.c.;d.Not used;e."Software" specially designed or modified for the operation of items specified in 9A012;f."Software" specially designed to design the internal cooling passages of aero gas turbine blades, vans and "tip shrouds";g."Software" having all of the following:1.Specially designed to predict aero thermal, aeromechanical and combustion conditions in aero gas turbine engines; and2.Theoretical modelling predictions of the aero thermal, aeromechanical and combustion conditions, which have been validated with actual aero gas turbine engine (experimental or production) performance data.	M19D1	"Software" which coordinates the function of more than one subsystem, specially designed or modified for "use" in the systems specified in 19.A.1. or 19.A.2.
9D101	"Software" specially designed or modified for the "use" of goods specified in 9B105, 9B106, 9B116 or 9B117.	M1D1	"Software" specially designed or modified for the "use" of "production facilities" specified in 1.B.
		M2D1	"Software" specially designed or modified for the "use" of "production facilities" specified in 2.B.1.
		M3D1	"Software" specially designed or modified for the "use" of "production facilities" and flow-forming machines specified in 3.B.1. or 3.B.3.
		M12D1	"Software" specially designed or modified for the "use" of equipment specified in 12.A.1.
		M15D1	"Software" specially designed or modified for the "use" of equipment specified in 15.B. usable for testing systems specified in 1.A., 19.A.1. or 19.A.2. or subsystems specified in 2.A. or 20.A.
		M20D1	"Software" specially designed or modified for the systems specified in 20.B.1.
9D103	"Software" specially designed for modelling, simulation or design integration of the space launch vehicles specified in 9A004, sounding rockets specified in 9A104 or "missiles", or the subsystemsspecified in 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119.Note:"Software" specified in 9D103 remains controlled when combined with specially designed hardware specified in 4A102.	M16D1	"Software" specially designed for modelling, simulation, or design integration of the systems specified in 1.A. or the subsystems specified in 2.A or 20.A.Technical Note:The modelling includes in particular the aerodynamic and thermodynamic analysis of the systems.
9D104	"Software" specially designed or modified for the "use" of goods specified in 9A001, 9A005, 9A006.d., 9A006.g., 9A007.a., 9A008.d., 9A009.a., 9A010.d., 9A011, 9A101, 9A102, 9A105, 9A106.c., 9A106.d., 9A107, 9A108.c., 9A109, 9A111, 9A115.a., 9A116.d., 9A117 or 9A118.	M2D2M2D4M3D2M2D5M20D2	"Software" specially designed or modified for the "use" of rocket motors or engines specified in 2.A.1.c."Software" specially designed or modified for the operation or maintenance of subsystems or equipment specified in 2.A.1.b.3."Software" specially designed or modified for the "use" of equipment specified in 3.A.1., 3.A.2., 3.A.4., 3.A.5., 3.A.6. or 3.A.9.Notes:1."Software" specially designed or modified for the "use" of engines specified in 3.A.1. may be exported as part of a manned aircraft or as replacement "software" therefor.2."Software" specially designed or modified for the "use" of propellant control systems specified in 3.A.5. may be exported as part of a satellite or as replacement "software" therefor."Software" specially designed or modified for the operation or maintenance of subsystems in 2.A.1.e."Software", not specified in 2.D.2., specially designed or modified for the "use" of rocket motors or engines specified in 20.A.1.b.
9D105	"Software" which coordinates the function of more than one subsystem, other than that specified in 9D003.e., specially designed or modified for "use" in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104 or "missiles".Technical Note:In 9D105 "missile" means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.	M1D2	"Software" specially designed or modified to coordinate the function of more than one subsystem in systems specified in 1.A.
		M19D1	"Software" which coordinates the function of more than one subsystem, specially designed or modified for "use" in the systems specified in 19.A.1. or 19.A.2.

9ETechnology

The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items		Missile Technology Control Regime (M.TCR): Equipment, software and technology annex
9E001	"Technology" according to the General Technology Note for the "development" of equipment	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
9E002	"Technology" according to the General Technology Note for the "production" of equipment materials, see 1E002.f.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
9E101	a."Technology" according to the General Technology Note for the "development" of goods specified in 9A101, 9A102, 9A104 to 9A111, 9A112.a. or 9A115 to 9A121.b."Technology" according to the General Technology Note for the "production" of "UAV"s specified in 9A012 or goods specified in 9A101, 9A102, 9A104 to 9A111, 9A112.a. or 9A115 to 9A121.Technical Note:In 9E101.b. "UAV" means unmanned aerial vehicle systems capable of a range exceeding 300 km.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".
9E102	"Technology" according to the General Technology Note for the "use" of space launch vehicles specified in9A004, goods specified in 9A005 to 9A011, "UAV"s specified in 9A012 or goods specified in 9A101, 9A102, 9A104 to 9A111, 9A112.a., 9A115 to 9A121, 9B105, 9B106, 9B115, 9B116, 9B117, 9D101 or 9D103.Technical Note:In 9E102 "UAV" means unmanned aerial vehicle systems capable of a range exceeding 300 km.	M	Means specific information which is required for the "development", "production" or "use" of a product. The information may take the form of "technical data" or "technical assistance".

ANNEX IV

List of "crude oil and petroleum products" referred to in articles 11 and 31(1)

HS Code	Description
2709 00	Petroleum oils and oils obtained from bituminous minerals, crude.
2710	Petroleum oils and oils obtained from bituminous minerals, other than crude; preparations not elsewhere specified or included, containing by weight 70 % or more of petroleum oils or of oils obtained from bituminous minerals, these oils being the basic constituents of the preparations; waste oils (save that the purchase, in Iran, of kerosene jet fuel of CN code 27101921 is not prohibited provided that it is intended and used solely for the purpose of the continuation of the flight operation of the aircraft into which it is loaded).
2712	Petroleum jelly; paraffin wax, microcrystalline petroleum wax, slack wax, ozokerite, lignite wax, peat wax, other mineral waxes, and similar products obtained by synthesis or by other processes, whether or not coloured.
2713	Petroleum coke, petroleum bitumen and other residues of petroleum oils or of oils obtained from bituminous minerals.
2714	Bitumen and asphalt, natural; bituminous or oil-shale and tar sands; asphaltites and asphaltic rocks.
2715 00 00	Bituminous mixtures based on natural asphalt, on natural bitumen, on petroleum bitumen, on mineral tar or on mineral tar pitch (for example, bituminous mastics, cut-backs).

ANNEX IVAProducts referred to in Articles 14a and 31(1)Natural gas and other gaseous hydrocarbons

HS code	Description
2709 00 10	Natural gas condensates
2711 11 00	Natural Gas – in liquefied state
2711 21 00	Natural Gas – in gaseous state
2711 12	Propane
2711 13	Butanes
2711 19 00	Other

ANNEX VList of 'petrochemical products' referred to in Articles 13 and 31(1)

HS code	Description
2812 10 94	Phosgene (carbonyl chloride)
2814	Ammonia
3102 30	Ammonium Nitrate
2901 21 00	Ethylene
2901 22 00	Propene (propylene)
2902 20 00	Benzene
2902 30 00	Toluene
2902 41 00	o-Xylene
2902 42 00	m-Xylene
2902 43 00	p-Xylene
2902 44 00	Mixed xylene isomers
2902 50 00	Styrene
2902 60 00	Ethyl benzene
2902 70 00	Cumene
2903 11 00	Chloromethane
2903 29 00	Unsaturated chlorinated derivatives of acyclic hydrocarbons - other
2903 81 00	Hexachlorocyclohexane [(HCH (ISO)], including lindane (ISO, DCI)
2903 82 00	Aldrin (ISO), chlordane (ISO) and heptachlor (ISO)
2903 89 90	Other halogenated derivatives of hydrocarbons
2903 91 00	Chlorobenzene, o-dichlorobenzene and p-dichlorobenzene
2903 92 00	Hexachlorobenzene (ISO) and DDT (ISO) [clofenotane (DCI), 1,1,1-trichloro-2,2-bis(p-chlorophenyl)ethane]
2903 99 90	Other halogenated derivatives of aromatic hydrocarbons
2909	Ether-alcohols and their halogenated, sulphonated, nitrated or nitrosated derivatives
2909 41	Oxydiethanol (diethylene glycol)
2909 43	Monobutyl ethers of ethylene-glycol or diethylene glycol
2909 44	Other monoalkyl ethers of ethylene-glycol or diethylene glycol
2909 49	Other ether-alcohols and their halogenated, sulphonated, nitrated or nitrosated derivatives
2905 11 00	Methanol (methyl alcohol)
2905 12 00	Propan-1-ol (propyl alcohol) and propan-2-ol (isopropyl alcohol
2905 13 00	Butan-1-ol (n-butyl alcohol)
2905 31 00	Ethylene glycol (ethanediol)
2907 11 – 2907 19	Phenols
2910 10 00	Oxirane (ethylene oxide)
2910 20 00	Methyloxirane (propylene oxide)
2914 11 00	Acetone
2917 14 00	Maleic anhydride (MA)
2917 35 00	Phthalic anhydride (PA)
2917 36 00	Terephthalic acid and its salts
2917 37 00	Dimethyl terephthalate (DMT)
2926 10 00	Acrylonitrile
Ex 2929 10 00	Methylene diphenyl diisocyanate (MDI)
Ex 2929 10 00	Hexamethylene diisocyanate (HDI)
Ex 2929 10 00	Toluene diisocyanate (TDI)
3901	Polymers of ethylene, in primary forms

HS code	Description
2707 10	Benzol (benzene)	All codes
2707 20	Toluol (toluene)	All codes
2707 30	Xylol (xylenes)	All codes
2707 40	Naphthalene	All codes
2707 99 80	Phenols
2711 14 00	Ethylene, propylene, butadiene

ANNEX VIList of key equipment and technology referred to in Articles 8 and 31(1)GENERAL NOTES1.The object of the prohibitions contained in this Annex should not be defeated by the export of any non-prohibited goods (including plant) containing one or more prohibited components when the prohibited component or components are the principal element of the goods and can feasibly be removed or used for other purposes.N.B.:In judging whether the prohibited component or components are to be considered the principal element, it is necessary to weigh the factors of quantity, value and technological know-how involved and other special circumstances which might establish the prohibited component or components as the principal element of the goods being procured.2.The goods specified in this Annex include both new and used goods.3.Definitions of terms between 'single quotation marks' are given in a technical note to the relevant item.4.Definitions of terms between "double quotation marks" can be found in Annex I to Regulation (EC) No 428/2009.GENERAL TECHNOLOGY NOTE (GTN)1.The "technology" "required" for the "development", "production" or "use" of prohibited goods remains under prohibition even when applicable to non-prohibited goods.2.Prohibitions do not apply to that "technology" which is the minimum necessary for the installation, operation, maintenance (checking) and repair of those goods which are not prohibited or the export of which has been authorised in accordance with Regulation (EC) No 423/2007 or this Regulation.3.Prohibitions on "technology" transfer do not apply to information "in the public domain", to "basic scientific research" or to the minimum necessary information for patent applications.EXPLORATION AND PRODUCTION OF CRUDE OIL AND NATURAL GAS1.AEquipment1.Geophysical survey equipment, vehicles, vessels and aircraft specially designed or adapted to acquire data for oil and gas exploration and specially designed components therefore.2.Sensors specially designed for downhole well operations in oil and gas wells, including sensors used for measurement whilst drilling and the associated equipment specially designed to acquire and store data from such sensors.3.Drilling equipment designed to drill rock formations, specifically for the purpose of exploring for, or producing oil, gas and other naturally occurring, hydrocarbon materials.4.Drill bits, drill pipes, drill collars, centralisers and other equipment, specially designed for use in and with oil and gas well drilling equipment.5.Drilling wellheads, 'blowout preventers' and 'Christmas or production trees' and the specially designed components thereof, meeting the 'API and ISO specifications' for use with oil and gas wells.Technical Notes:a.A 'blowout preventer' is a device typically used at ground level (or if drilling underwater, at the seabed) during drilling to prevent the uncontrolled escape of oil and/or gas from the well.b.A 'Christmas tree or production tree' is a device typically used to control flow of fluids from the well when it is complete and oil and/or gas production has started.c.For the purpose of this item, 'API and ISO specifications' refers to the American Petroleum Institute specifications 6A, 16A, 17D and 11IW and/or the International Standards Organisation specifications 10423 and 13533 for blowout preventers, wellhead and Christmas trees for use on oil and/or gas wells.6.Drilling and production platforms for crude oil and natural gas.7.Vessels and barges incorporating drilling and/or petroleum processing equipment used for producing oil, gas and other naturally occurring flammable materials.8.Liquid/gas separators meeting API specification 12J, specially designed to process the production from an oil or gas well, to separate the petroleum liquids from any water and any gas from the liquids.9.Gas compressor with a design pressure of 40 bar (PN 40 and/or ANSI 300) or more and having a suction volume capacity of 300000 Nm3/h or more, for the initial processing and transmission of natural gas, excluded gas compressors for CNG (Compressed Natural Gas) filling stations, and specially designed components therefore.10.Subsea production control equipment and the components thereof meeting 'API and ISO specifications' for use with oil and gas wells.Technical Note:For the purposes of this entry, 'API and ISO specifications' refers to the American Petroleum Institute specification 17 F and/or the International Standards Organisation specification 13268 for subsea production control systems.11.Pumps, typically high capacity and/or high pressure (in excess of 0,3 m3 per minute and/or 40 bar), specially designed to pump drilling muds and/or cement into oil and gas wells.1.BTest and inspection equipment1.Equipment specially designed for sampling, testing and analysing the properties of drilling mud, oil well cements and other materials specially designed and/or formulated for use in oil and gas wells.2.Equipment specially designed for sampling, testing and analysing the properties of rock samples, liquid and gaseous samples and other materials taken from an oil and/or gas well either during or after drilling, or from the initial processing facilities attached thereto.3.Equipment specially designed for collecting and interpreting information about the physical and mechanical condition of an oil and/or gas well, and for determining the in situ properties of the rock and reservoir formation.1.CMaterials1.Drilling mud, drilling mud additives and the components thereof, specially formulated to stabilise oil and gas wells during drilling, to recover drill cuttings to the surface and to lubricate and cool the drilling equipment in the well.2.Cements and other materials meeting the 'API and ISO specifications' for use in oil and gas wells.Technical Note:'API and ISO specification' refers to the American Petroleum Institute specification 10A or the International Standards Organisation specification 10426 for oil well cements and other materials specially formulated for use in the cementing of oil and gas wells.3.Corrosion inhibiting, emulsion treatment, defoaming agents and other chemicals specially formulated to be used in the drilling for, and the initial processing of, petroleum produced from an oil and/or gas well.1.DSoftware1."Software" specially designed to collect and interpret data acquired from seismic, electromagnetic, magnetic or gravity surveys for the purpose of establishing oil or gas prospectivity.2."Software" specially designed for storing, analysing and interpreting information acquired during drilling and production to assess the physical characteristics and behaviour of oil or gas reservoirs.3."Software" specially designed for the "use" of petroleum production and processing facilities or specific sub-units of such facilities.1.ETechnology1."Technology" "required" for the "development", "production" and "use" of equipment specified in 1.A.01 – 1.A.11.REFINING OF CRUDE OIL AND LIQUEFACTION OF NATURAL GAS2.AEquipment1.Heat exchangers as follows and specially designed components therefore:a.Plate-fin heat exchangers with a surface/volume ratio greater than 500 m2/m3, specially designed for pre-cooling of natural gas;b.Coil-wound heat exchangers specially designed for liquefaction or sub-cooling of natural gas.2.Cryogenic pumps for the transport of media at a temperature below – 120 °C having a transport capacity of more than 500 m3/h and specially designed components therefore.3.'Coldbox' and 'coldbox' equipment not specified by 2.A.1.Technical Note:'Coldbox' equipment' refers to a specially designed construction, which is specific for LNG plants and incorporates the process stage of liquefaction. The 'coldbox' comprises heat exchangers, piping, other instrumentation and thermal insulators. The temperature inside the 'coldbox' is below – 120 °C (conditions for condensation of natural gas). The function of the 'coldbox' is the thermal insulation of the above described equipment.4.Equipment for shipping terminals of liquefied gases having a temperature below – 120 °C and specially designed components therefore.5.Flexible and non-flexible transfer line having a diameter greater than 50 mm for the transport of media below – 120 °C.6.Maritime vessels specially designed for the transport of LNG.7.Electrostatic desalters specially designed to remove contaminants such as salts, solids and water from crude oil and specially designed components therefore.8.All crackers, including hydrocrackers, and cokers, specially designed for conversion of vacuum gas oils or vacuum residuum, and specially designed components therefore.9.Hydrotreaters specially designed for desulphurisation of gasoline, diesel cuts and kerosene and specially designed components therefore.10.Catalytic reformers specially designed for conversion of desulphurised gasoline into high-octane gasoline, and specially designed components therefore.11.Refinery units for C5-C6 cuts isomerisation, and refinery units for alkylation of light olefins, to improve the octane index of the hydrocarbon cuts.12.Pumps specially designed for the transport of crude oil and fuels, having a capacity of 50 m3/h or more and specially designed components therefore.13.Tubes with an outer diameter of 0,2 m or more and made from any of the following materials:a.Stainless steels with 23 % chromium or more by weight;b.Stainless steels and nickel bases alloys with a 'Pitting resistance equivalent' number higher than 33.Technical Note:'Pitting resistance equivalent' (PRE) number characterises the corrosion resistance of stainless steels and nickel alloys to pitting or crevice corrosion. The pitting resistance of stainless steels and nickel alloys is primarily determined by their compositions, primarily: chromium, molybdenum, and nitrogen. The formula to calculate the PRE number is: 14.'Pigs' (Pipeline Inspection Gauge(s)) and specially designed components therefore.15.'Pig' launchers and 'pig' catchers for the integration or removing of 'pigs'Technical Note:'Pig' is a device typically used for cleaning or inspection of a pipeline from inside (corrosion state or crack formation) and is propelled by the pressure of the product in the pipeline.16.Tanks for the storage of crude oil and fuels with a volume greater than 1000 m3 (1000000 litres) as follows, and specially designed components therefore:a.fixed roof tanks;b.floating roof tanks.17.Subsea flexible pipes specially designed for the transportation of hydrocarbons and injection fluids, water or gas, having a diameter greater than 50 mm.18.Flexible pipes used for high pressure for topside and subsea application.19.Isomeration equipment specially designed for production of high-octane gasoline based on light hydrocarbons as feed, and specially designed components therefore.2.BTest and inspection equipment1.Equipment specially designed for testing and analysing of quality (properties) of crude oil and fuels.2.Interface control systems specially designed for controlling and optimising of the desalting process.2.CMaterials1.Diethyleneglycol (CAS 111-46-6), Triethylene glycol (CAS 112-27-6)2.N-Methylpyrrolidon (CAS 872-50-4), Sulfolane (CAS 126-33-0)3.Zeolites, of natural or synthetic origin, specially designed for fluid catalytic cracking or for the purification and/or dehydration of gases, including natural gases.4.Catalysts for the cracking and conversion of hydrocarbons as follows:a.Single metal (platinum group) on alumina type or on zeolite, specially designed for catalytic reforming process;b.Mixed metal species (platinum in combination with other noble metals) on alumina type or on zeolite, specially designed for catalytic reforming process;c.Cobalt and nickel catalysts doped with molybdenum on alumina type or on zeolite, specially designed for catalytic desulphurisation process;d.Palladium, nickel, chromium and tungsten catalysts on alumina type or on zeolite, specially designed for catalytic hydrocracking process.5.Gasoline additives specially formulated for increasing the octane number of gasoline.Note:This entry includes Ethyl tertiary butyl ether(ETBE) (CAS 637-92-3) and Methyl tertiary butyl ether (MTBE) CAS 1634-04-4).2.DSoftware1."Software" specially designed for the "use" of LNG plants or specific sub-units of such plants.2."Software" specially designed for the "development", "production" or "use" of plants (including their sub-units) for oil refining.2.ETechnology1."Technology" "required" for the "development", "production" or "use" of equipment for the conditioning and purification of raw natural gas (dehydration, sweetening, removal of impurities).2."Technology" for the liquefaction of natural gas, including "technology" required for the "development", "production" or "use" of LNG plants.3."Technology" "required" for the "development", "production" or "use" of equipment for the shipment of liquefied natural gas.4."Technology" "required" for the "development", "production" or "use" of maritime vessels specially designed for the transport of liquefied natural gas.5."Technology" "required" for the "development", "production" or "use" of tanks for the storage of crude oil and fuels.6."Technology" "required" for the "development", "production" or "use" of a refinery plant, such as:6.1."Technology" for conversion of light olefin to gasoline;6.2.Catalytic reforming and isomerisation technology;6.3.Catalytic and thermal cracking technology.PETROCHEMICAL INDUSTRY3.AEquipment1.Reactorsa.specially designed for production of phosgene (CAS 506-77-4) and specially designed components therefor;b.for phosgenation specially designed for the production of HDI, TDI, MDI and specially designed components therefor, with the exception of secondary reactors;c.specially designed for low pressure (up to max 40 bar) polymerisation of ethylene and propylene and specially designed components therefore;d.specially designed for the thermal cracking of EDC (ethylene dichloride) and specially designed components therefor, with the exception of secondary reactors;e.specially designed for chlorination and oxychlorination in the production of vinyl chloride and specially designed components therefor, with the exception of secondary reactors;2.Thin film evaporators and falling film evaporators consisting of materials resistant to hot concentrated acetic acid and specially designed components therefor, and the relevant software developed therefor;3.Plants for the separation of hydrochloric acid by electrolysis and specially designed components therefore, and the relevant software developed therefor;4.Columns having a diameter larger than 5000 mm and specially designed components therefor;5.Ball valves and plug valves with ceramic balls or plugs, having a nominal diameter of 10 mm or more, and specially designed components therefor;6.Centrifugal and/or reciprocating compressor having an installed power above 2 MW and meeting specification API 617 or API 618;3.BTest and inspection equipment3.CMaterials1.Catalysts applicable to processes of production of trinitrotoluene, ammonium nitrate and other chemical and petrochemical processes used for explosive manufacturing, and the relevant software developed therefor;2.Catalysts used for the production of monomers such as ethylene and propylene (steam cracking units and/or Gas to petrochemicals units), and the relevant software developed therefor;3.DSoftware1."Software" specially designed for the "development", "production" or "use" of equipment specified in 3.A;2."Software" specially designed for the "use" in methanol plants;3.ETechnology1."Technology" for the "development", "production" or "use" of Gas-To-Liquid (GTL) or Gas-To-Petrochemicals (GTP) processes or for GTL- or GTP- plants;2."Technology" "required" for the "development", "production" or "use" of equipment designed for the manufacture of ammonia and methanol plants;3."Technology" for the "production" of MEG (Mono ethylene glycol), EO (Ethylene oxide)/EG (Ethylene glycol)Note:"Technology" means specific information necessary for the "development", "production" or "use" of goods. This information takes the form of "technical data" or "technical assistance".ANNEX VIA

Key equipment and technology referred to Articles 8, 10(1)(c) and 31(1)

HS code	Description
	– Casing, tubing and drill pipe, of a kind used in drilling for oil or gas:
7304 22	– Drill pipe of stainless steel
7304 23	– – Other drill pipe
7304 24	– – Other, of stainless steel
7304 29	– – Other
ex 7305	Other tubes and pipes (for example, welded, riveted or similarly closed), having circular cross-sections, the external diameter of which exceeds 406,4 mm, of iron or steel, with a chrome content of 1 % or more and with a cold resistance that can go below -120°C
	– Line pipe of a kind used for oil or gas pipelines:
7306 11	– – Welded, of stainless steel
7306 19	– – Other
	– Casing and tubing of a kind used in drilling for oil or gas:
7306 21 00	– – Welded, of stainless steel
7306 29 00	– – Other
	Containers for compressed or liquefied gas, of iron or steel:
7311 00 99	– Other, of a capacity of 1000 l or more
ex 7613	Aluminium containers for compressed or liquefied gas, of a capacity of 1000 l or more

ANNEX VIB

Key equipment and technology referred to in Articles 10a, 10b, 10c and 31(1)

HS code	Description
8406 10 00	Steam turbines for marine propulsion
ex 8406 90	Parts of steam turbines for marine propulsion
8407 21	Marine propulsion engines, outboard motors
ex 8407 29	Marine propulsion engines, other
8408 10	Marine propulsion engines
ex 8409 91 00	Parts suitable for use solely or principally with machines of subheadings 8407 21 or 8407 29
ex 8409 99 00	Parts suitable for use solely or principally with machines of subheading 8408 10
ex 8411 81	Other gas turbine of a power not exceeding 5000 kW, for marine propulsion
ex 8411 82	Other gas turbines of a power exceeding 5000 kW, for marine propulsion
ex 8468	Machinery and apparatus for soldering, brazing or welding whether or not capable of cutting, other than those of heading 8515; gas-operated surface tempering machines and appliances:
ex 8483	Transmission shafts (including cam shafts and crank shafts) and cranks; bearing housings and plain shaft bearings; gears and gearing; ball or roller screws; gear boxes and other speed changers, including torque converters; flywheels and pulleys, including pulley blocks; clutches and shaft couplings (including universal joints), designed for the propulsion of vessels at the maximum possible deadweight tonnage at scantling draught of 55000 dwt or more
8487 10	Ships' or boats' propellers and blades therefor
ex 8515	Electric (including electrically heated gas), laser or other light or photon beam, ultrasonic, electron beam, magnetic pulse or plasma arc soldering, brazing or welding machines and apparatus, whether or not capable of cutting; electric machines and apparatus for hot spraying of metals or cermets:
ex 9014 10 00	Direction finding compasses, solely for the maritime industry
ex 9014 80 00	Other navigational instruments and appliances, solely for the maritime industry
ex 9014 90 00	Parts and accessories of subheadings 9014 10 00 and 9014 80 00, solely for the maritime industry
ex 9015	Surveying (including photogram metrical surveying), hydro graphic, oceanographic, hydrological, meteorological or geophysical instruments and appliances, excluding compasses; rangefinders, solely for the maritime industry.

ANNEX VII

List of gold, precious metals and diamonds referred to in Articles 15 and 31(1)

HS Code	Description
7102	Diamonds, whether or not worked, but not mounted or set
7106	Silver (including silver plated with gold or platinum), unwrought or in semi-manufactured forms, or in powder form
7108	Gold (including gold plated with platinum), unwrought or in semi-manufactured forms, or in powder form
7109	Base metals or silver, clad with gold, not further worked than semi-manufactured.
7110	Platinum, unwrought or in semi-manufactured forms, or in powder form
7111	Base metals, silver or gold, clad with platinum, not further worked than semi-manufactured.
7112	Waste and scrap of precious metal or of metal clad with precious metal; other waste and scrap containing precious metal or precious-metal compounds, of a kind used principally for the recovery of precious metal

ANNEX VIIASoftware referred to in Article 10d1.Enterprise Resource Planning software, designed specifically for use in nuclear and military industriesExplanatory note:Enterprise Resource Planning software is software used for financial accounting, management accounting, human resources, manufacturing, supply chain management, project management, customer relationship management, data services, or access control.ANNEX VIIBGraphite and raw, fabricated semi-finished metals referred to in Article 15aHS Codes and descriptions1.Raw or semi-fabricated graphite

2504	Natural graphite
3801	Artificial graphite; colloidal or semi-colloidal graphite; preparations based on graphite or other carbon in the form of pastes, blocks, plates or other semi-manufactures

2.Corrosion-resistant high-grade steel (Chromium-content > 12 %) in form of sheet, plate, tube or bar

ex 72 19	Flat-rolled products of stainless steel, of a width of 600 mm or more
ex 72 20	Flat-rolled products of stainless steel, of a width of less than 600 mm
ex 72 21	Bars and rods, hot-rolled, in irregularly wound coils, of stainless steel
ex 72 22	Other bars and rods of stainless steel; angles, shapes and sections of stainless steel
ex 72 25	Flat-rolled products of other alloy steel, of a width of 600 mm or more
ex 72 26	Flat-rolled products of other alloy steel, of a width of less than 600 mm
ex 72 27	Bars and rods, hot-rolled, in irregularly wound coils, of other alloy steel
ex 72 28	Other bars and rods of other alloy steel; angles, shapes and sections, of other alloy steel; hollow drill bars and rods, of alloy or non-alloy steel
ex 73 04	Tubes, pipes and hollow profiles, seamless, of iron (other than cast iron) or steel
ex 73 05	Other tubes and pipes (for example, welded, riveted or similarly closed), having circular cross-sections, the external diameter of which exceeds 406,4 mm, of iron or steel
ex 73 06	Other tubes, pipes and hollow profiles (for example, open seam or welded, riveted or similarly closed), of iron or steel
ex 73 07	Tube or pipe fittings (for example, couplings, elbows, sleeves), of iron or steel

3.Aluminium and alloys in form of sheet, plate, tube or bar

ex 76 04	Aluminium bars, rods and profiles
ex 7604 10 10	–Of aluminium, not alloyed
	– –Bars and rods
ex 7604 29 10	–Of aluminium alloys
	– –Hollow profiles
	– – –Bars and rods
7606	Aluminium plates, sheets and strip, of a thickness exceeding 0,2 mm
7608	Aluminium tubes and pipes
7609	Aluminium tube or pipe fittings (for example, couplings, elbows, sleeves)

4.Titanium and alloys in form of sheet, plate, tube or bar

ex 8108 90	Titanium and articles thereof, including waste and scrap
	–Other

5.Nickel and alloys in form of sheet, plate, tube or bar

ex 75 05	Nickel bars, rods, profiles and wire
ex 7505 11	Bar and Rods
ex 7505 12
7506	Nickel plates, sheets, strip and foil
ex 75 07	Nickel tubes, pipes and tube or pipe fittings (for example, couplings, elbows, sleeves)
7507 11	–Tubes and pipes
	– –Of nickel, not alloyed
7507 12	–Tubes and pipes
	– –Of nickel alloys
7507 20	–Tube or pipe fittings

Explanatory note: the metal alloys in points 2, 3, 4 and 5 are those containing a higher percentage by weight of the stated metal than of any other element.ANNEX VIIIList of persons and entities referred to in Article 23(1)A.Persons and entities involved in nuclear or ballistic missiles activitiesNatural persons(1)Fereidoun Abbasi-Davani. Function: Senior Ministry of Defence and Armed Forces Logistics (MODAFL) Scientist. DOB: (a) 1958 (b) 1959. POB: Abadan, Iran (Islamic Republic of). Other information: Has "links to the Institute of Applied Physics. Working closely with Mohsen Fakhrizadeh-Mahabadi."Date of UN designation: 24.3.2007.(2)Dawood Agha-Jani. Function: Head of the PFEP - Natanz. Other information: Person involved in Iran's nuclear programme.Date of UN designation: 23.12.2006.(3)Ali Akbar Ahmadian. Title: Vice Admiral. Function: Chief of Iranian Revolutionary Guard Corps (IRGC) Joint Staff. DOB: 1961. POB: Kerman, Iran (Islamic Republic of). A.k.a.: Ali Akbar Ahmedian. Other information: position changed.Date of UN designation: 24.3.2007.(4)Amir Moayyed Alai. Other information: involved in managing the assembly and engineering of centrifuges.Date of EU designation: 24.4.2007 (UN: 3.3.2008).(5)Behman Asgarpour. Function: Operational Manager (Arak). Other information: Person involved in Iran's nuclear programme.Date of UN designation: 23.12.2006.(6)Mohammad Fedai Ashiani. Other information: involved in the production of ammonium uranyl carbonate and management of the Natanz enrichment complex.Date of EU designation: 24.4.2007 (UN: 3.3.2008).(7)Abbas Rezaee Ashtiani. Other information: a senior official at the AEOI Office of Exploration and Mining Affairs.Date of UN designation: 3.3.2008.(8)Bahmanyar Morteza Bahmanyar. Function: Head of Finance & Budget Department of the Aerospace Industries Organisation (AIO). DOB: 31 December 1952. Nationality: Iran. Passport no: (a) I0005159, issued in Iran (b) 10005159, issued in Iran.Date of UN designation: 23.12.2006.(9)Haleh Bakhtiar. Other information: involved in the production of magnesium at a concentration of 99,9 %.Date of EU designation: 24.4.2007 (UN: 3.3.2008).(10)Morteza Behzad. Other information: involved in making centrifuge components.Date of EU designation: 24.4.2007 (UN: 3.3.2008).(11)Ahmad Vahid Dastjerdi. Function: Head of the Aerospace Industries Organisation (AIO). DOB: 15 January 1954. Passport no: A0002987, issued in Iran. Other information: Served as Deputy Defence Minister.Date of UN designation: 23.12.2006.(12)Ahmad Derakhshandeh. Function: Chairman and Managing Director of Bank Sepah, which provides support for the AIO and subordinates, including SHIG and SBIG, both of which were designated under resolution 173 (2006). DOB: 11 August 1956. Address: 33 Hormozan Building, Pirozan St., Sharaj Ghods, Tehran, Iran (Islamic Republic of).Date of UN designation: 24.3.2007.(13)Mohammad Eslami. Title: Dr. Other information: Head of Defence Industries Training and Research Institute. A.k.a.: Mohammad Islami; Mohamed Islami; Mohammed Islami. Other information: Served as Deputy Defence Minister from 2012 to 2013.Date of UN designation: 3.3.2008.(14)Reza-Gholi Esmaeli. Function: Head of Trade & International Affairs Dept, Aerospace Industries Organisation (AIO). DOB: 3 April 1961. A.k.a.: Reza-Gholi Ismaili. Passport no: A0002302, issued in Iran (Islamic Republic of).Date of UN designation: 23.12.2006.(15)Mohsen Fakhrizadeh-Mahabadi. Senior MODAFL scientist and former head of the Physics Research Centre (PHRC). Passport no: (a) A0009228 (Unconfirmed (likely Iran)) (b) 4229533 (Unconfirmed (likely Iran)). Other information: The IAEA have asked to interview him about the activities of the PHRC over the period he was head but Iran has refused.Date of UN designation: 24.3.2007.(16)Mohammad Hejazi. Title: Brigadier General. Function: Commander of Bassij resistance force. DOB: 1959. POB: Isfahan, Iran (Islamic Republic of). A.k.a.: Mohammed Hijazi.Date of UN designation: 24.3.2007.(17)Mohsen Hojati. Function: Head of Fajr Industrial Group, which is designated under resolution 1737(2006) for its role in the ballistic missile programme. DOB: 28 September 1955. Passport no: G4506013, issued in Iran (Islamic Republic of).Date of UN designation: 24.3.2007.(18)Seyyed Hussein Hosseini. Other information: AEOI official involved in the heavy water research reactor project at Arak.Date of EU designation: 24.4.2007 (UN: 3.3.2008).(19)M. Javad Karimi Sabet. Other information: Head of Novin Energy Company, which is designated under resolution 1747 (2007).Date of EU designation: 24.4.2007 (UN: 3.3.2008).(20)Mehrdada Akhlaghi Ketabachi. Function: Head of Shahid Bagheri Industrial Group (SBIG), which is designated under resolution 1737(2006) for its role in the ballistic missile programme. DOB: 10 September 1958. Passport no: A0030940, issued in Iran (Islamic Republic of).Date of UN designation: 24.3.2007.(21)Ali Hajinia Leilabadi. Function: Director General of Mesbah Energy Company. Other information: Person involved in Iran's nuclear programme.Date of UN designation: 23.12.2006.(22)Naser Maleki. Function: Head of Shahid Hemmat Industrial Group (SHIG), which is designated under resolution 1737(2006) for its role in Iran's ballistic missile programme. DOB: 1960. Passport no: A0003039 issued in Iran (Islamic Republic of). National identification no: Iran (Islamic Republic of) 0035-11785, issued in Iran (Islamic Republic of). Other information: Naser Maleki is also a MODAFL official overseeing work on the Shahab-3 ballistic missile programme. The Shahab-3 is Iran's long-range ballistic missile currently in service.Date of UN designation: 24.3.2007.(23)Hamid-Reza Mohajerani. Other information: involved in production management at the Uranium Conversion Facility (UCF) at Esfahan.Date of EU designation: 24.4.2007 (UN: 3.3.2008).(24)Jafar Mohammadi. Function: Technical Adviser to the Atomic Energy Organisation of Iran (AEOI) (in charge of managing the production of valves for centrifuges). Other information: Person involved in Iran's nuclear programme.Date of UN designation: 23.12.2006.(25)Ehsan Monajemi. Function: Construction Project Manager, Natanz. Other information: Person involved in Iran's nuclear programme.Date of UN designation: 23.12.2006.(26)Mohammad Reza Naqdi. Title: Brigadier-General. DOB: (a) 11 February 1949 (b) 11 February 1952 (c) 11 February 1953 (d) 11 February 1961. POB: (a) Najaf, Iraq (b) Tehran, Iran (Islamic Republic of). Other information: former Deputy Chief of Armed Forces General Staff for Logistics and Industrial Research. Head of State Anti-Smuggling Headquarters, engaged in efforts to get round the sanctions imposed by UNSCR 1737 (2006) and 1747 (2007).Date of UN designation: 3.3.2008.(27)Houshang Nobari. Other information: involved in the management of the Natanz enrichment complex.Date of EU designation: 24.4.2007 (UN: 3.3.2008).(28)Mohammad Mehdi Nejad Nouri. Title: Lieutenant General. Function: Rector of Malek Ashtar University of Defence Technology. Other information: The chemistry department of Ashtar University of Defence Technology, affiliated to MODALF and has conducted experiments on beryllium. Deputy Minister of Science, Research and Technology.Date of UN designation: 23.12.2006.(29)Mohammad Qannadi. Function: AEOI Vice President for Research & Development. Other information: Person involved in Iran's nuclear programme.Date of UN designation: 23.12.2006.(30)Amir Rahimi. Function: Head of Esfahan Nuclear Fuel Research and Production Center. Other information: Esfahan Nuclear Fuel Research and Production Center is part of the AEOI's Nuclear Fuel Production and Procurement Company, which is involved in enrichment-related activities.Date of UN designation: 24.3.2007.(31)Javad Rahiqi: Function: Head of the Atomic Energy Organization of Iran (AEOI) Esfahan Nuclear Technology Center (additional information: DOB: 24 April 1954; POB: Marshad).Date of UN designation: 9.6.2010 (EU: 24.4.2007).(32)Abbas Rashidi. Other information: involved in enrichment work at Natanz.Date of EU designation: 24.4.2007 (UN: 3.3.2008).(33)Morteza Rezaie. Title: Brigadier General. Function: Deputy Commander of IRGC. DOB: 1956. A.k.a.: Mortaza Rezaie; Mortaza Rezai; Morteza Rezai.Date of UN designation: 24.3.2007.(34)Morteza Safari. Title: Rear Admiral. Function: Commander of IRGC Navy. A.k.a.: Mortaza Safari; Morteza Saferi; Murtaza Saferi; Murtaza Safari.Date of UN designation: 24.3.2007.(35)Yahya Rahim Safavi. Title: Major General. Function: Commander, IRGC (Pasdaran). DOB: 1952. POB: Isfahan, Iran (Islamic Republic of). A.k.a.: Yahya Raheem Safavi.Date of UN designation: 23.12.2006.(36)Seyed Jaber Safdari. Other information: Manager of the Natanz Enrichment Facilities.Date of UN designation: 24.3.2007.(37)Hosein Salimi. Title: General. Function: Commander of the Air Force, IRGC (Pasdaran). A.k.a.: Husain Salimi; Hosain Salimi; Hussain Salimi; Hosein Saleemi; Husain Saleemi; Hosain Saleemi; Hussain Saleemi; Hossein Salimi; Hossein Saleemi. Passport no: D08531177, issued in Iran (Islamic Republic of).Date of UN designation: 23.12.2006.(38)Qasem Soleimani. Title: Brigadier General. Function: Commander of Qods force. DOB: 11 March 1957. POB: Qom, Iran (Islamic Republic of). A.k.a.: Qasim Soleimani; Qasem Sulaimani; Qasim Sulaimani; Qasim Sulaymani; Qasem Sulaymani; Kasim Soleimani; Kasim Sulaimani; Kasim Sulaymani; Haj Qasem; Haji Qassem; Sarder Soleimani. Passport no: 008827, issued in Iran. Other information: Promoted to Major General, retaining his position as Commander of Qods Force.Date of UN designation: 24.3.2007.(39)Ghasem Soleymani. Other information: Director of Uranium Mining Operations at the Saghand Uranium Mine.Date of UN designation: 3.3.2008.(40)Mohammad Reza Zahedi. Title: Brigadier General. Function: Commander of IRGC Ground Forces. DOB: 1944. POB: Isfahan, Iran (Islamic Republic of). A.k.a.: Mohammad Reza Zahidi; Mohammad Raza Zahedi.Date of UN designation: 24.3.2007.(41)Mohammad Baqer Zolqadr. Function: General, IRGC officer, Deputy Interior Minister for Security Affairs. A.k.a.: Mohammad Bakr Zolqadr; Mohammad Bakr Zolkadr; Mohammad Baqer Zolqadir; Mohammad Baqer Zolqader.Date of UN designation: 24.3.2007.(42)Azim Aghajani. Function: Member of the IRGC-Qods Force operating under the direction of Qods Force Commander, Major General Qasem Soleimani, who was designated by the UN Security Council in Resolution 1747 (2007). A.k.a.: Azim Adhajani; Azim Agha-Jani. Nationality: Iran (Islamic Republic of). Passport no: (a) 6620505 issued in Iran (Islamic Republic of) (b) 9003213 issued in Iran (Islamic Republic of). Other information: facilitated a breach of paragraph 5 of Resolution 1747 (2007) prohibiting the export of arms and related materiel from Iran.Date of UN designation: 18.4.2012(43)Ali Akbar Tabatabaei. Function: Member of the IRGC Qods Force operating under the direction of Qods Force Commander, Major General Qasem Soleimani, who was designated by the UN Security Council in Resolution 1747 (2007). DOB: 1967. A.k.a.: (a) Sayed Akbar Tahmaesebi; Syed Akber Tahmaesebi (b) Ali Akber Tabatabaei; Ali Akber Tahmaesebi; Ali Akbar Tahmaesebi. Nationality: Iran (Islamic Republic of). Passport no: (a) 9003213 issued in Iran/unknown (b) 6620505 issued in Iran/unknown. Other information: facilitated a breach of paragraph 5 of Resolution 1747 (2007) prohibiting the export of arms and related materiel from Iran.Date of UN designation: 18.4.2012Entities(1)Abzar Boresh Kaveh Co. (alias BK Co.). Other information: involved in the production of centrifuge components.Date of UN designation: 3.3.2008.(2)Amin Industrial Complex: Amin Industrial Complex sought temperature controllers which may be used in nuclear research and operational/production facilities. Amin Industrial Complex is owned or controlled by, or acts on behalf of, the Defense Industries Organization (DIO), which was designated in resolution 1737 (2006).Location: P.O. Box 91735-549, Mashad, Iran; Amin Industrial Estate, Khalage Rd., Seyedi District, Mashad, Iran; Kaveh Complex, Khalaj Rd., Seyedi St., Mashad, IranA.K.A.: Amin Industrial Compound and Amin Industrial Company.Date of UN designation: 9.6.2010.(3)Ammunition and Metallurgy Industries Group (AMIG) A.k.a. Ammunition Industries Group. Other information: (a) AMIG controls 7th of Tir, which is designated under resolution 1737 (2006) for its role in Iran's centrifuge programme. AMIG is in turn owned and controlled by DIO, which is designated under resolution 1737 (2006).Date of UN designation: 24.3.2007.(4)Armament Industries Group: Armament Industries Group (AIG) manufacturers and services a variety of small arms and light weapons, including large- and medium-calibre guns and related technology. AIG conducts the majority of its procurement activity through Hadid Industries Complex.Location: Sepah Islam Road, Karaj Special Road Km 10, Iran; Pasdaran Ave., P.O. Box 19585/777, Tehran, Iran.Date of EU designation: 24.4.2007 (UN: 9.6.2010).(5)Atomic Energy Organisation of Iran (AEOI). Other information: Involved in Iran's nuclear programme.Date of UN designation: 23.12.2006.(6)Bank Sepah and Bank Sepah International. Other information: Bank Sepah provides support for the Aerospace Industries Organisation (AIO) and subordinates, including Shahid Hemmat Industrial Group (SHIG) and Shahid Bagheri Industrial Group (SBIG).Date of UN designation: 24.3.2007.(7)Barzagani Tejarat Tavanmad Saccal companies. Other information: (a) subsidiary of Saccal System companies, (b) this company tried to purchase sensitive goods for an entity listed in resolution 1737 (2006).Date of UN designation: 3.3.2008.(8)Cruise Missile Industry Group. A.k.a. Naval Defense Missile Industry Group. Other information: Production and development of cruise missiles. Responsible for naval missiles including cruise missiles.Date of UN designation: 3.3.2008.(9)Defence Industries Organisation (DIO). Other information: Overarching MODAFL-controlled entity, some of whose subordinates have been involved in the centrifuge programme making components, and in the missile programme.Date of UN designation: 23.12.2006.(10)Defense Technology and Science Research Center: Defense Technology and Science Research Center (DTSRC) is owned or controlled by, or acts on behalf of, Iran's Ministry of Defense and Armed Forces Logistics (MODAFL), which oversees Iran's defence R&D, production, maintenance, exports, and procurement.Location: Pasdaran Ave, PO Box 19585/777, Tehran, Iran.Date of EU designation: 24.4.2007 (UN: 9.6.2010).(11)Doostan International Company: Doostan International Company (DICO) supplies elements to Iran's ballistic missile program.Date of UN designation: 9.6.2010.(12)Electro Sanam Company (alias (a) E. S. Co., (b) E. X. Co.). Other information: AIO front-company, involved in the ballistic missile programme.Date of UN designation: 3.3.2008.(13)Esfahan Nuclear Fuel Research and Production Centre (NFRPC) and Esfahan Nuclear Technology Centre (ENTC). Other information: They are parts of the Atomic Energy Organisation of Iran's (AEOI) Nuclear Fuel Production and Procurement Company.Date of UN designation: 24.3.2007.(14)Ettehad Technical Group. Other information: AIO front-company, involved in the ballistic missile programme.Date of UN designation: 3.3.2008.(15)Fajr Industrial Group. Other information: (a) Instrumentation Factory Plant, (b) Subordinate entity of AIO.Date of UN designation: 23.12.2006.(16)Farasakht Industries: Farasakht Industries is owned or controlled by, or act on behalf of, the Iran Aircraft Manufacturing Company, which in turn is owned or controlled by MODAFL.Location: P.O. Box 83145-311, Kilometer 28, Esfahan-Tehran Freeway, Shahin Shahr, Esfahan, Iran.Date of UN designation: 9.6.2010.(17)Farayand Technique. Other information: (a) Involved in Iran's nuclear programme (centrifuge programme), (b) Identified in IAEA reports.Date of UN designation: 23.12.2006.(18)First East Export Bank, P.L.C.: First East Export Bank, PLC is owned or controlled by, or acts on behalf of, Bank Mellat. Over the last seven years, Bank Mellat has facilitated hundreds of millions of dollars in transactions for Iranian nuclear, missile, and defense entities.Location: Unit Level 10 (B1), Main Office Tower, Financial Park Labuan, Jalan Merdeka, 87000 WP Labuan, Malaysia; Business Registration Number LL06889 (Malaysia).Date of UN designation: 9.6.2010.(19)Industrial Factories of Precision (IFP) Machinery (alias Instrumentation Factories Plant). Other information: used by AIO for some acquisition attempts.Date of UN designation: 3.3.2008.(20)Jabber Ibn Hayan. Other information: AEOI laboratory involved in fuel-cycle activities.Date of UN designation: 3.3.2008 (EU: 24.4.2007).(21)Joza Industrial Co. Other information: AIO front-company, involved in the ballistic missile programme.Date of UN designation: 3.3.2008.(22)Kala-Electric. A.k.a.: Kalaye Electric. Other information: Provider for PFEP — Natanz.Date of UN designation: 23.12.2006.(23)Karaj Nuclear Research Centre. Other information: Part of AEOI's research division.Date of UN designation: 24.3.2007.(24)Kaveh Cutting Tools Company: Kaveh Cutting Tools Company is owned or controlled by, or acts on behalf of, the DIO.Location: 3rd Km of Khalaj Road, Seyyedi Street, Mashad 91638, Iran; Km 4 of Khalaj Road, End of Seyedi Street, Mashad, Iran; P.O. Box 91735-549, Mashad, Iran; Khalaj Rd., End of Seyyedi Alley, Mashad, Iran; Moqan St., Pasdaran St., Pasdaran Cross Rd., Tehran, Iran.Date of UN designation: 9.6.2010.(25)Kavoshyar Company. Other information: Subsidiary company of AEOI.Date of UN designation: 24.3.2007.(26)Khorasan Metallurgy Industries. Other information: (a) subsidiary of the Ammunition Industries Group (AMIG) which depends on DIO, (b) involved in the production of centrifuge components.Date of UN designation: 3.3.2008.(27)M. Babaie Industries: M. Babaie Industries is subordinate to Shahid Ahmad Kazemi Industries Group (formally the Air Defense Missile Industries Group) of Iran's Aerospace Industries Organization (AIO). AIO controls the missile organizations Shahid Hemmat Industrial Group (SHIG) and the Shahid Bakeri Industrial Group (SBIG), both of which were designated in resolution 1737 (2006).Location: P.O. Box 16535-76, Tehran, 16548, Iran.Date of UN designation: 9.6.2010.(28)Malek Ashtar University: A subordinate of the DTRSC within MODAFL. This includes research groups previously falling under the Physics Research Center (PHRC). IAEA inspectors have not been allowed to interview staff or see documents under the control of this organization to resolve the outstanding issue of the possible military dimension to Iran's nuclear program.Location: Corner of Imam Ali Highway and Babaei Highway, Tehran, Iran.Date of EU designation: 24.6.2008 (UN: 9.6.2010).(29)Mesbah Energy Company. Other information: (a) Provider for A40 research reactor - Arak, (b) Involved in Iran's nuclear programme.Date of UN designation: 23.12.2006.(30)Ministry of Defense Logistics Export: Ministry of Defense Logistics Export (MODLEX) sells Iranian-produced arms to customers around the world in contravention of resolution 1747 (2007), which prohibits Iran from selling arms or related materiel.Location: PO Box 16315-189, Tehran, Iran; located on the west side of Dabestan Street, Abbas Abad District, Tehran, Iran.Date of EU designation: 24.6.2008 (UN: 9.6.2010).(31)Mizan Machinery Manufacturing: Mizan Machinery Manufacturing (3M) is owned or controlled by, or acts on behalf of, SHIG.Location: P.O. Box 16595-365, Tehran, IranA.K.A.: 3MGDate of EU designation: 24.6.2008 (UN: 9.6.2010).(32)Modern Industries Technique Company: Modern Industries Technique Company (MITEC) is responsible for design and construction of the IR-40 heavy water reactor in Arak. MITEC has spearheaded procurement for the construction of the IR-40 heavy water reactor.Location: Arak, IranA.K.A.: Rahkar Company, Rahkar Industries, Rahkar Sanaye Company, Rahkar Sanaye NovinDate of UN designation: 9.6.2010.(33)Nuclear Research Center for Agriculture and Medicine: The Nuclear Research Center for Agriculture and Medicine (NFRPC) is a large research component of the Atomic Energy Organization of Iran (AEOI), which was designated in resolution 1737 (2006). The NFRPC is AEOI's center for the development of nuclear fuel and is involved in enrichment-related activities.Location: P.O. Box 31585-4395, Karaj, IranA.K.A.: Center for Agricultural Research and Nuclear Medicine; Karaji Agricultural and Medical Research CenterDate of UN designation: 9.6.2010.(34)Niru Battery Manufacturing Company. Other information: (a) subsidiary of the DIO, (b) its role is to manufacture power units for the Iranian military including missile systems.Date of UN designation: 3.3.2008.(35)Novin Energy Company (alias Pars Novin). Other information: It operates within AEOI.Date of UN designation: 24.3.2007.(36)Parchin Chemical Industries. Other information: Branch of DIO, which produces ammunition, explosives, as well as solid propellants for rockets and missiles.Date of UN designation: 24.3.2007.(37)Pars Aviation Services Company. Other information: maintains various aircraft, including MI-171, used by IRGC Air Force.Date of UN designation: 24.3.2007.(38)Pars Trash Company. Other information: (a) Involved in Iran's nuclear programme (centrifuge programme), (b) Identified in IAEA reports.Date of UN designation: 23.12.2006.(39)Pejman Industrial Services Corporation: Pejman Industrial Services Corporation is owned or controlled by, or acts on behalf of, SBIG.Location: P.O. Box 16785-195, Tehran, Iran.Date of UN designation: 9.6.2010.(40)Pishgam (Pioneer) Energy Industries. Other information: has participated in construction of the Uranium Conversion Facility at Esfahan.Date of UN designation: 3.3.2008.(41)Qods Aeronautics Industries. Other information: It produces unmanned aerial vehicles (UAVs), parachutes, paragliders, para-motors, etc. IRGC has boasted to use these products as part of its asymmetric warfare doctrine.Date of UN designation: 24.3.2007.(42)Sabalan Company: Sabalan is a cover name for SHIG.Location: Damavand Tehran Highway, Tehran, Iran.Date of UN designation: 9.6.2010.(43)Sanam Industrial Group. Other information: subordinate to AIO, which has purchased equipment on AIO's behalf for the missile programme.Date of UN designation: 24.3.2007.(44)Safety Equipment Procurement (SEP). Other information: AIO front-company, involved in the ballistic missile programme.Date of UN designation: 3.3.2008.(45)7th of Tir. Other information: Subordinate of DIO, widely recognised as being directly involved in Iran's nuclear programme.Date of UN designation: 23.12.2006.(46)Sahand Aluminum Parts Industrial Company (SAPICO): SAPICO is a cover name for SHIG.Location: Damavand Tehran Highway, Tehran, Iran.Date of UN designation: 9.6.2010.(47)Shahid Bagheri Industrial Group (SBIG). Other information: Subordinate entity of AIO.Date of UN designation: 23.12.2006.(48)Shahid Hemmat Industrial Group (SHIG). Other information: Subordinate entity of AIO.Date of UN designation: 23.12.2006.(49)Shahid Karrazi Industries: Shahid Karrazi Industries is owned or controlled by, or act on behalf of, SBIG.Location: Tehran, Iran.Date of UN designation: 9.6.2010.(50)Shahid Satarri Industries: Shahid Sattari Industries is owned or controlled by, or acts on behalf of, SBIG.Location: Southeast Tehran, IranA.K.A.: Shahid Sattari Group Equipment Industries.Date of UN designation: 9.6.2010.(51)Shahid Sayyade Shirazi Industries: Shahid Sayyade Shirazi Industries (SSSI) is owned or controlled by, or acts on behalf of, the DIO.Location: Next To Nirou Battery Mfg. Co, Shahid Babaii Expressway, Nobonyad Square, Tehran, Iran; Pasdaran St., P.O. Box 16765, Tehran 1835, Iran; Babaei Highway — Next to Niru M.F.G, Tehran, Iran.Date of UN designation: 9.6.2010.(52)Sho'a' Aviation. Other information: It produces micro-lights, which IRGC has claimed it is using as part of its asymmetric warfare doctrine.Date of UN designation: 24.3.2007.(53)Special Industries Group: Special Industries Group (SIG) is a subordinate of DIO.Location: Pasdaran Avenue, PO Box 19585/777, Tehran, Iran.Date of EU designation: 24.7.2007 (UN: 9.6.2010).(54)TAMAS Company. Other information: (a) involved in enrichment-related activities, (b) TAMAS is an overarching body, under which four subsidiaries have been established, including one for uranium extraction to concentration and another in charge of uranium processing, enrichment and waste.Date of EU designation: 24.4.2007 (UN: 3.3.2008).(55)Tiz Pars: Tiz Pars is a cover name for SHIG. Between April and July 2007, Tiz Pars attempted to procure a five axis laser welding and cutting machine, which could make a material contribution to Iran's missile program, on behalf of SHIG.Location: Damavand Tehran Highway, Tehran, Iran.Date of UN designation: 9.6.2010.(56)Ya Mahdi Industries Group. Other information: subordinate to AIO, which is involved in international purchase of missile equipment.Date of UN designation: 24.3.2007.(57)Yazd Metallurgy Industries: Yazd Metallurgy Industries (YMI) is a subordinate of DIO.Location: Pasdaran Avenue, Next To Telecommunication Industry, Tehran 16588, Iran; Postal Box 89195/878, Yazd, Iran; P.O. Box 89195-678, Yazd, Iran; Km 5 of Taft Road, Yazd, Iran.A.K.A.: Yazd Ammunition Manufacturing and Metallurgy Industries, Directorate of Yazd Ammunition and Metallurgy IndustriesDate of UN designation: 9.6.2010.(58)Behineh Trading Co.Other information: An Iranian company that played a key role in Iran’s illicit transfer of arms to West Africa and acted on behalf of the IRGC Qods Force, commanded by Major General Qasem Soleimani, designated by the UN Security Council in Resolution 1747 (2007), as the shipper of the weapons consignment.Additional information: Location: Tavakoli Building, Opposite of 15th Alley, Emam-Jomeh Street, Tehran, Iran. Telephone: +98 9195382305. Website: http://www.behinehco.irDate of UN designation: 18 April 2012.(59)Yas Air: Yas Air is the new name for Pars Air, a company that was owned by Pars Aviation Services Company, which in turn was designated by the United Nations Security Council in Resolution 1747 (2007). Yas Air has assisted Pars Aviation Services Company, a United Nations-designated entity, in violating paragraph 5 of Resolution 1747 (2007).Location: Mehrabad International Airport, Next to Terminal No. 6, Tehran, Iran.Date of UN designation: 10.12.2012.(60)SAD Import Export Company: SAD Import Export Company has assisted Parchin Chemical Industries and 7th of Tir Industries, a United Nations-designated entity, in violating paragraph 5 of Resolution 1747 (2007).Location: Haftom Tir Square, South Mofte Avenue, Tour Line No 3/1, Tehran, Iran. (2) P.O. Box 1584864813.Date of UN designation: 10.12.2012.B.Entities owned, controlled, or acting on behalf of the Iranian Revolutionary Guard Corps(1)Fater (or Faater) Institute: Khatam al-Anbiya (KAA) subsidiary. Fater has worked with foreign suppliers, likely on behalf of other KAA companies on IRGC projects in Iran.Date of UN designation: 9.6.2010.(2)Gharagahe Sazandegi Ghaem: Gharagahe Sazandegi Ghaem is owned or controlled by KAADate of UN designation: 9.6.2010.(3)Ghorb Karbala: Ghorb Karbala is owned or controlled by KAA.Date of UN designation: 9.6.2010.(4)Ghorb Nooh: Ghorb Nooh is owned or controlled by KAA.Date of UN designation: 9.6.2010.(5)Hara Company: Owned or controlled by Ghorb Nooh.Date of UN designation: 9.6.2010.(6)Imensazan Consultant Engineers Institute: Owned or controlled by, or acts on behalf of, KAA.Date of UN designation: 9.6.2010.(7)Khatam al-Anbiya Construction Headquarters: Khatam al-Anbiya Construction Headquarters (KAA) is an IRGC-owned company involved in large scale civil and military construction projects and other engineering activities. It undertakes a significant amount of work on Passive Defense Organization projects. In particular, KAA subsidiaries were heavily involved in the construction of the uranium enrichment site at Qom/Fordow.Date of UN designation: 9.6.2010.(8)Makin: Makin is owned or controlled by or acting on behalf of KAA, and is a subsidiary of KAA.Date of UN designation: 9.6.2010.(9)Omran Sahel: Owned or controlled by Ghorb Nooh.Date of UN designation: 9.6.2010.(10)Oriental Oil Kish: Oriental Oil Kish is owned or controlled by or acting on behalf of KAA.Date of UN designation: 9.6.2010.(11)Rah Sahel: Rah Sahel is owned or controlled by or acting on behalf of KAA.Date of UN designation: 9.6.2010.(12)Rahab Engineering Institute: Rahab is owned or controlled by or acting on behalf of KAA, and is a subsidiary of KAA.Date of UN designation: 9.6.2010.(13)Sahel Consultant Engineers: Owned or controlled by Ghorb Nooh.Date of UN designation: 9.6.2010.(14)Sepanir: Sepanir is owned or controlled by or acting on behalf of KAA.Date of UN designation: 9.6.2010.(15)Sepasad Engineering Company: Sepasad Engineering Company is owned or controlled by or acting on behalf of KAA.Date of UN designation: 9.6.2010.C.Entities owned, controlled, or acting on behalf of the Islamic Republic of Iran Shipping Lines (IRISL)(1)Irano Hind Shipping Company:Location: 18 Mehrshad Street, Sadaghat Street, Opposite of Park Mellat, Vali-e-Asr Ave., Tehran, Iran; 265, Next to Mehrshad, Sedaghat St., Opposite of Mellat Park, Vali Asr Ave., Tehran 1A001, IranDate of UN designation: 9.6.2010.(2)IRISL Benelux NV:Location: Noorderlaan 139, B-2030, Antwerp, Belgium; V.A.T. Number BE480224531 (Belgium)Date of UN designation: 9.6.2010.(3)South Shipping Line Iran (SSL):Location: Apt. No. 7, 3rd Floor, No. 2, 4th Alley, Gandi Ave., Tehran, Iran; Qaem Magham Farahani St., Tehran, IranDate of UN designation: 9.6.2010.ANNEX IXList of persons and entities referred to in Article 23(2)I.Persons and entities involved in nuclear or ballistic missile activities and persons and entities providing support to the Government of Iran

A.Persons

	Name	Identifying information	Reasons	Date of listing
1.	Reza AGHAZADEH	DoB: 15.03.1949Passport number: S4409483 valid 26.04.2000 – 27.04.2010: Issued: Tehran,Diplomatic passport number: D9001950, issued on 22.01.2008 valid until 21.01.2013, Place of birth: Khoy	Former Head of the Atomic Energy Organisation of Iran (AEOI). The AEOI oversees Iran's nuclear programme and is designated under UNSCR 1737 (2006).	23.4.2007
2.	Ali DIVANDARI (a.k.a DAVANDARI)		Head of Bank Mellat (see Part B, no 4)	26.7.2010
3.	Dr Hoseyn (Hossein) FAQIHIAN	Address of NFPC: AEOI-NFPD, P.O.Box: 11365-8486, Tehran/Iran	Deputy and Director-General of the Nuclear Fuel Production and Procurement Company (NFPC) (see Part B, no 30), part of the AEOI. The AEOI oversees Iran's nuclear programme and is designated under UNSCR 1737 (2006). The NFPC is involved in enrichment-related activities that Iran is required by the IAEA Board and Security Council to suspend.	23.4.2007
4.	Engineer Mojtaba HAERI		MODAFL Deputy for Industry. Supervisory role over AIO and DIO	23.6.2008
5.	Mahmood JANNATIAN	DoB 21.04.1946,passport number: T12838903	Deputy Head of the Atomic Energy Organisation of Iran	23.6.2008
6.	Said Esmail KHALILIPOUR (a.k.a.: LANGROUDI)	DoB: 24.11.1945,PoB: Langroud	Deputy Head of AEOI. The AEOI oversees Iran's nuclear programme and is designated under UNSCR 1737 (2006).	23.4.2007
7.	Ali Reza KHANCHI	Address of NRC: AEOI-NRC P.O.Box: 11365-8486 Tehran/ Iran;Fax: (+9821) 8021412	Head of AEOI's Tehran Nuclear Research Centre. The IAEA is continuing to seek clarification from Iran about plutonium separation experiments carried out at the TNRC, including about the presence of HEU particles in environmental samples taken at the Karaj Waste Storage Facility where containers used to store depleted uranium targets used in those experiments are located. The AEOI oversees Iran's nuclear programme and is designated under UNSCR 1737 (2006).	23.4.2007
8.	Ebrahim MAHMUDZADEH		Managing Director of Iran Electronic Industries (see Part B, no 20)	23.6.2008
9.	Fereydoun MAHMOUDIAN	Born on 07.11.1943 in Iran.Passport no 05HK31387 issued on 01.01.2002 in Iran, valid until 07.08.2010.Acquired French nationality on 07.05.2008	Director of Fulmen (see Part B, No 13)	26.7.2010
10.	Brigadier-General Beik MOHAMMADLU		MODAFL Deputy for Supplies and Logistics (see Part B, no 29)	23.6.2008
11.	Mohammad MOKHBER	4th Floor, No 39 Ghandi street TehranIran 1517883115	President of the Setad Ejraie foundation, an investment fund linked to Ali Khameneï, the Supreme Leader. Member of the Management Board of Sina Bank.	26.7.2010
12.	Mohammad Reza MOVASAGHNIA		Head of Samen Al A'Emmeh Industries Group (SAIG), also known as the Cruise Missile Industry Group. This organisation was designated under UNSCR 1747 and listed in Annex I to Common Position 2007/140/CFSP.	26.7.2010
13.	Anis NACCACHE		Administrator of Barzagani Tejarat Tavanmad Saccal companies; his company has attempted to procure sensitive goods for entities designated under Resolution 1737 (2006).	23.6.2008
14.	Brigadier-General Mohammad NADERI		Head of Iran's Aviation Industries Organisation (IAIO). Former Head of Iran's Aerospace Industries Organisation (AIO). AIO has taken part in sensitive Iranian programmes.	23.6.2008
15.	Ali Akbar SALEHI		Minister for Foreign Affairs. Former Head of the Atomic Energy Organisation of Iran (AEOI). The AEOI oversees Iran's nuclear programme and is designated under UNSCR 1737 (2006).	17.11.2009
16.	Rear Admiral Mohammad SHAFI'I RUDSARI		Former MODAFL Deputy for Coordination (see Part B, no 29).	23.6.2008
17.	Abdollah SOLAT SANA		Managing Director of the Uranium Conversion Facility (UCF) in Esfahan. This is the facility that produces the feed material (UF6) for the enrichment facilities at Natanz. On 27 August 2006, Solat Sana received a special award from President Ahmadinejad for his role.	23.4.2007
18.	Mohammad AHMADIAN		Formerly acting Head of the Atomic Energy Organisation of Iran (AEOI), and currently Deputy Head of the AEOI. The AEOI oversees Iran's nuclear programme and is designated under UNSCR 1737 (2006).	23.05.2011
19.	Engineer Naser RASTKHAH		Deputy Head of the AEOI. The AEOI oversees Iran's nuclear programme and is designated under UNSCR 1737 (2006).	23.05.2011
20.	Behzad SOLTANI		Deputy Head of the AEOI. The AEOI oversees Iran's nuclear programme and is designated under UNSCR 1737 (2006).	23.05.2011
21.	Massoud AKHAVAN-FARD		Deputy Head of the AEOI for Planning, International and Parliamentary affairs. The AEOI oversees Iran's nuclear programme and is designated under UNSCR 1737 (2006).	23.05.2011
22.	Dr Ahmad AZIZI		Deputy Chairman and Managing Director of EU-designated Melli Bank PLC.	1.12.2011
23.	Davoud BABAEI		The current head of security for the Ministry Of Defence Armed Forces Logistics' research institute the Organisation of Defensive Innovation and Research (SPND), which is run by UN-designated Mohsen Fakhrizadeh-Mahabadi. The IAEA have identified SPND with their concerns over possible military dimensions to Iran's nuclear programme over which Iran refuses to co-operate. As head of security, Babaei is responsible for preventing the disclosure of information including to the IAEA.	1.12.2011
24.	Hassan BAHADORI		Chief Executive Officer of EU-designated Arian Bank	1.12.2011
25.	Sayed Shamsuddin BORBORUDIa.k.a. Seyed Shamseddin BORBOROUDI	DOB: 21 September 1969	Deputy Head of UN designated Atomic Energy Organisation of Iran, where he is subordinate to UN designated Feridun Abbasi Davani. Has been involved in the Iranian nuclear programme since at least 2002, including as the former head of procurement and logistics at AMAD, where he was responsible for using front companies such as Kimia Madan to procure equipment and material for Iran's nuclear weapons programme.	1.12.2011
26.	Dr Peyman Noori BROJERDI		Chairman of the Board and Managing Director of EU-designated Bank Refah	1.12.2011
27.	Kamran DANESHJOO (a.k.a. DANESHJOU)		Former Minister of Science, Research and Technology. He has provided support for Iran's proliferation-sensitive nuclear activities.	1.12.2011
28.	Dr Abdolnaser HEMMATI		Managing Director and Chief Executive Officer of EU-designated Banque Sina	1.12.2011
29.	Milad JAFARI	date of birth 20.9.74	An Iranian national supplying goods, mostly metals, to UN designated SHIG front companies. Delivered goods to SHIG between January and November 2010. Payments for some of the goods were made at the central branch of EU-designated Export Development Bank of Iran (EDBI) in Tehran after November 2010.	1.12.2011
30.	Dr Mohammad JAHROMI		Chairman and Managing Director of EU-designated Bank Saderat	1.12.2011
31.	Ali KARIMIAN		An Iranian national supplying goods, mostly carbon fibre to UN-designated SHIG and SBIG.	1.12.2011
32.	Majid KHANSARI		Managing Director of UN-designated Kalaye Electric Company.	1.12.2011
33.	Mahmoud Reza KHAVARI		Chairman of the Board and Managing Director of EU-designated Bank Melli.	1.12.2011
34.	Mohammad Reza MESKARIAN		The London Chief Executive Officer of EU-designated Persia International Bank	1.12.2011
35.	Mohammad MOHAMMADI		Managing Director of MATSA.	1.12.2011
36.	Dr M H MOHEBIAN		Managing Director of EU-designated Post Bank.	1.12.2011
37.	Mohammad Sadegh NASERI		Head of the Physics Research Institute (formerly known as the Institute of Applied Physics).	1.12.2011
38.	Mohammad Reza REZVANIANZADEH		Managing Director of the EU-designated Nuclear Reactors Fuel Company (SUREH). He is also an AEOI official. He oversees and issues tenders to procurement companies for sensitive procurement work required at the Fuel Manufacturing Plant (FMP), the Zirconium Powder Plant (ZPP) and the Uranium Conversion Facility (UCF).	1.12.2011
39.	A SEDGHI		Chairman and Non-executive Director of the EU-designated Melli Bank PLC	1.12.2011
40.	Hamid SOLTANI		Managing Director of the EU-designated Management Company for Nuclear Power Plant Construction (MASNA)	1.12.2011
41.	Bahman VALIKI		Chairman of the Board and Managing Director of the EU-designated Export Development Bank of Iran.	1.12.2011
42.	Javad AL YASIN		Head of the Research Centre for Explosion and Impact, also known as METFAZ	1.12.2011
43.	S ZAVVAR		Acting General Manager in Dubai of the EU-designated Persia International Bank.	1.12.2011
44.	Majid NAMJOO	Born on 5 January 1963 in Tehran, Iran	Minister of Energy. Member of the Supreme National Security Council, which formulates Iran's nuclear policy.	16.10.2012
45.	Babak Zanjani	Date of birth: 12 March 1971	Babak Zanjani has provided support for the financing of transactions in Iranian crude oil conducted by the Iranian Ministry of Petroleum, which is designated by the EU. In addition, he has assisted the Central Bank of Iran and the National Iranian Oil Company (NIOC), which are also designated by the EU, to evade the EU's restrictive measures.He has been a facilitator for Iranian oil transactions and has made transfers of oil-related funds, notably through Naftiran Intertrade Company (NICO) and Hong Kong Intertrade, which are controlled by the Iranian Government and also designated by the EU.In addition, he provided essential services to the Iranian Revolutionary Guard Corps (IRGC) by enabling transfers of funds for the benefit of Khatam al-Anbiya, an IRGC-owned company subject to UN and EU sanctions.	8.11.2014

B.EntitiesIn accordance with Council Implementing Regulation (EU) 2016/603, this entry shall apply until 22 October 2016.Information erased within the framework of the protection of individuals with regard to the processing of personal data.Information erased within the framework of the protection of individuals with regard to the processing of personal data.Information erased within the framework of the protection of individuals with regard to the processing of personal data.Information erased within the framework of the protection of individuals with regard to the processing of personal data.Information erased within the framework of the protection of individuals with regard to the processing of personal data.Information erased within the framework of the protection of individuals with regard to the processing of personal data.Information erased within the framework of the protection of individuals with regard to the processing of personal data.Information erased within the framework 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	Name	Identifying information	Reasons	Date of listing
1.	Aerospace Industries Organisation, AIO	AIO, 28 Shian 5, Lavizan, Tehran, IranLangare Street,Nobonyad Square,Tehran, Iran	AIO oversees Iran's production of missiles, including Shahid Hemmat Industrial Group, Shahid Bagheri Industrial Group and Fajr Industrial Group, which were all designated under UNSCR 1737 (2006). The head of AIO and two other senior officials were also designated under UNSCR 1737 (2006)	23.4.2007
2.	Armed Forces Geographical Organisation		Assessed to provide geospatial data for the Ballistic Missile programme	23.6.2008
3.	Azarab Industries	Ferdowsi Ave, PO Box 11365-171, Tehran, Iran	Energy sector firm that provides manufacturing support to the nuclear programme, including designated proliferation sensitive activities. Involved in the construction of the Arak heavy-water reactor.	26.7.2010
4.	Bank Mellat (including all branches) and subsidiaries	Head Office Building, 327 Takeghani (Taleghani) Avenue, Tehran 15817, Iran;P.O. Box 11365-5964, Tehran 15817, Iran	Bank Mellat engages in a pattern of conduct which supports and facilitates Iran's nuclear and ballistic missile programmes. It has provided banking services to UN and EU listed entities or to entities acting on their behalf or at their direction, or to entities owned or controlled by them. It is the parent bank of First East Export Bank which is designated under UNSCR 1929.	26.7.2010
	(a)Mellat Bank SB CJSC	P.O. Box 24, Yerevan 0010, Republic of Armenia	100 % owned by Bank Mellat	26.7.2010
	(b)
5.	Bank Melli, Bank Melli Iran (including all branches) and subsidiaries	Ferdowsi Avenue, PO Box 11365-171, Tehran, Iran	Providing or attempting to provide financial support for companies which are involved in or procure goods for Iran's nuclear and missile programmes (AIO, SHIG, SBIG, AEOI, Novin Energy Company, Mesbah Energy Company, Kalaye Electric Company and DIO). Bank Melli serves as a facilitator for Iran's sensitive activities. It has facilitated numerous purchases of sensitive materials for Iran's nuclear and missile programmes. It has provided a range of financial services on behalf of entities linked to Iran's nuclear and missile industries, including opening letters of credit and maintaining accounts. Many of the above companies have been designated by UNSCRs 1737 (2006) and 1747 (2007).Bank Melli continues in this role, by engaging in a pattern of conduct which supports and facilitates Iran's sensitive activities. Using its banking relationships, it continues to provide support for, and financial services to, UN and EU listed entities in relation to such activities. It also acts on behalf of, and at the direction of such entities, including Bank Sepah, often operating through their subsidiaries and associates.	23.6.2008
	(a)Arian Bank (a.k.a. Aryan Bank)	House 2, Street Number 13, Wazir Akbar Khan, Kabul, Afghanistan	Arian Bank is a joint-venture between Bank Melli and Bank Saderat.	26.7.2010
	(b)Assa Corporation	ASSA CORP, 650 (or 500) Fifth Avenue, New York, USA; Tax ID No. 1368932 (United States)	Assa Corporation is a front company created and controlled by Bank Melli. It was set up by Bank Melli to channel money from the United States to Iran.	26.7.2010
	(c)Assa Corporation Ltd	6 Britannia Place, Bath Street, St Helier JE2 4SU, Jersey Channel Islands	Assa Corporation Ltd is the parent organization of Assa Corporation. Owned or controlled by Bank Melli	26.7.2010
	(d)Bank Kargoshaie (a.k.a. Bank Kargoshaee, a.k.a Kargosai Bank, a.k.a Kargosa'i Bank)	587 Mohammadiye Square, Mowlavi St., Tehran 11986, Iran	Bank Kargoshaee is owned by Bank Melli.	26.7.2010
	(e)Bank Melli Iran Investment Company (BMIIC)	No 1 - Didare ShomaliHaghani Highway 1518853115 Tehran Iran;Alt. Location:No.2, Nader Alley, Vali-Asr Str., Tehran, Iran, P.O. Box 3898-15875;Alt. Location:Bldg 2, Nader Alley after Beheshi Forked Road, P.O. Box 15875-3898, Tehran, Iran 15116;Alt., Location:Rafiee Alley, Nader Alley, 2 After Serahi Shahid Beheshti, Vali E Asr Avenue, Tehran, Iran;Business Registration Number: 89584.	Affiliated with entities sanctioned by the United States, the European Union or the United Nations since 2000. Designated by the United States for being owned or controlled by Bank Melli.	26.7.2010
	(f)Bank Melli Iran ZAO (a.k.a. Mir Business Bank)	Number 9/1, Ulitsa Mashkova, Moscow, 130064, Russia Alternative addr: Mashkova st. 9/1 Moscow 105062 Russia	Owned by Bank Melli.	23.6.2008
	(g)Bank Melli Printing and Publishing Company (BMPPC)	18th Km Karaj Special Road, 1398185611 Tehran, Iran, P.O. Box 37515-183;Alt. Location:Km 16 Karaj Special Road, Tehran, Iran;Business Registration Number 382231	Designated by the United States for being owned or controlled by Bank Melli	26.7.2010
	(h)Cement Investment and Development Company (CIDCO) (a.k.a.: Cement Industry Investment and Development Company, CIDCO, CIDCO Cement Holding)	No 20, West Nahid Blvd.Vali Asr Ave.Tehran, Iran, 1967757451No. 241, Mirdamad Street, Tehran, Iran	Wholly owned by Bank Melli Investment Co. Holding Company to manage all cement companies owned by BMIIC	26.7.2010
	(i)First Persian Equity Fund	Walker House, 87 Mary Street, George Town, Grand Cayman, KY1-9002, Cayman Islands;Alt. Location:Clifton House, 7z5 Fort Street, P.O. Box 190, Grand Cayman, KY1-1104; Cayman Islands;Alt. Location:Rafi Alley, Vali Asr Avenue, Nader Alley, Tehran, 15116, Iran, P.O.Box 15875-3898	Cayman-based fund licensed by the Iranian Government for foreign investment in the Tehran Stock Exchange	26.7.2010
	(j)Mazandaran Cement Company	No 51, sattari st.Afric Ave.TehranIranAlt. Loc.:Africa Street, Sattari Street No. 40, P.O. Box 121, Tehran, Iran 19688;Alt Location:40 Satari Ave. Afrigha Highway, P.O. Box 19688, Tehran, Iran	Controlled by Bank Melli Iran	26.7.2010
	(k)Mehr Cayman Ltd.	Cayman Islands; Commercial Registry Number 188926 (Cayman Islands)	Owned or controlled by Bank Melli	26.7.2010
	(l)Melli Agrochemical Company PJS (a.k.a: Melli Shimi Keshavarz)	5th Floor No 2315th Street, Gandi Ave. Vanak Sq., Tehran, IranAlt. Loc.:Mola Sadra Street, 215 Khordad, Sadr Alley No. 13, Vanak Sq., P.O. Box 15875-1734, Tehran, Iran	Owned or controlled by Bank Melli	26.7.2010
	(m)Melli Bank plc	London Wall, 11th floor, London EC2Y 5EA, United Kingdom	Owned by Bank Melli.	23.6.2008
	(n)Melli Investment Holding International	514 Business Avenue Building, Deira, P.O. Box 181878, Dubai, United Arab Emirates;Registration Certificate Number (Dubai) 0107 issued 30. Nov 2005.	Owned or controlled by Bank Melli	26.7.2010
	(o)Shemal Cement Company (a.k.a: Siman Shomal, a.k.a Shomal Cement Company )	No 269 Dr Beheshti Ave. P.O. Box 15875/4571 Tehran - 15146 IranAlt. Loc.:Dr Beheshti Ave No. 289, Tehran, Iran 151446;Alt. Location:289 Shahid Baheshti Ave., P.O. Box 15146, Tehran, Iran	Controlled by Bank Melli Iran	26.7.2010
6.
7.
	(a)Bank Saderat PLC (London)	5 Lothbury, London, EC2R 7 HD, UK	100 % owned subsidiary of Bank Saderat
7a.
	(a)Bank Saderat PLC (London)	5 Lothbury, London, EC2R 7 HD, UK	100 % owned subsidiary of Bank Saderat
8.	Sina Bank	No. 187, Avenue Motahhari Ave., Teheran, 1587998411, IranTel: +9821 88532434-7, +9821 88532434-6E-mail: infor@sinabank.irWebsite: http://www.sinabank.ir/	Sina Bank is controlled by the Mostazafan Foundation, a major Iranian parastatal entity directly controlled by the Supreme Leader, and which has an 84 % shareholding in Sina Bank. It provides financial services to the Mostazafan Foundation and its group of subsidiary units and companies. Accordingly, Sina Bank provides financial support to the Government of Iran through the Mostazafan Foundation.	26.7.2010
9.	ESNICO (Equipment Supplier for Nuclear Industries Corporation)	No. 1, 37th Avenue, Asadabadi Street, Tehran, Iran	Procures industrial goods, specifically for the nuclear programme activities carried out by AEOI, Novin Energy and Kalaye Electric Company (all designated under UNSCR 1737). ESNICO's Director is Haleh Bakhtiar (designated in UNSCR 1803).	26.7.2010
10.	Etemad Amin Invest Co Mobin	Pasadaran Av. Tehran, Iran	Close to Naftar and to Bonyad-e Mostazafan, Etemad Amin Invest Co Mobin contributes to funding the strategic interests of the regime and of the parallel Iranian state.	26.7.2010
11.
12.	Fajr Aviation Composite Industries	Mehrabad Airport, PO Box 13445-885, Tehran, Iran	A subsidiary of the IAIO within MODAFL both designated by the EU which primarily produces composite materials for the aircraft industry.	26.7.2010
13.	Fulmen	167 Darya boulevard - Shahrak Ghods, 14669 - 8356 Tehran.	Fulmen was involved in the installation of electrical equipment on the Qom/Fordoo site before its existence had been revealed.	26.7.2010
	(a)Arya Niroo Nik		Arya Niroo Nik is a front company used by Fulmen for some of its operations.	26.7.2010
14.	Future Bank BSC	Block 304. City Centre Building. Building 199, Government Avenue, Road 383, Manama, Bahrain. PO Box 785;Business Registration 2k Document: 54514-1 (Bahrain) expires 9 Jun 2009; Trade License No 13388 (Bahrain)	Two-thirds of Bahrain-based Future Bank are owned by Iranian banks. EU-designated Bank Melli and Bank Saderat each own one-third of the shares, the remaining third being held by Ahli United Bank (AUB) of Bahrain. Although AUB still owns its shares of Future Bank, according to its 2007 annual report, AUB no longer exercises significant influence over the bank which is effectively controlled by its Iranian parents both of which are singled out in UNSCR 1803 as Iranian banks requiring particular 'vigilance'. The tight links between Future Bank and Iran are further evidenced by the fact that the Chairman of Bank Melli has also held concurrently the position of Chairman of Future Bank.	26.7.2010
15.	Industrial Development & Renovation Organization (IDRO)		Government body responsible for acceleration of Iran's industrialisation. Controls various companies involved in work for the nuclear and missile programmes and involved in the foreign procurement advanced manufacturing technology in order to support them.	26.7.2010
16.	Iran Aircraft Industries (IACI)		A subsidiary of the IAIO within MODAFL (see no 29). Manufactures, repairs, and conducts overhauls of airplanes and aircraft engines and procures aviation-related parts often of US-origin typically via foreign intermediaries. IACI and its subsidiaries have also been detected using a worldwide network of brokers seeking to procure aviation-related goods.	26.7.2010
17.	Iran Aircraft Manufacturing Company (a.k.a: HESA, HESA Trade Center, HTC, IAMCO, IAMI, Iran Aircraft Manufacturing Company, Iran Aircraft Manufacturing Industries, Karkhanejate Sanaye Havapaymaie Iran, Hava Peyma Sazi-e Iran, Havapeyma Sazhran, Havapeyma Sazi Iran, Hevapeimasazi)	P.O. Box 83145-311, 28 km Esfahan – Tehran Freeway, Shahin Shahr, Esfahan, Iran;P.O. Box 14155-5568, No. 27 Ahahamat Ave., Vallie Asr Square, Tehran 15946, Iran;P.O. Box 81465-935, Esfahan, Iran;Shahih Shar Industrial Zone, Isfahan, Iran; P.O. Box 8140, No. 107 Sepahbod Gharany Ave., Tehran, Iran	Owned or controlled by, or acts on behalf of; MODAFL (see no 29).	26.7.2010
18.	Iran Centrifuge Technology Company (a.k.a. TSA or TESA)	156 Golestan Street, Saradr-e Jangal, Tehran	Iran Centrifuge Technology Company has taken over the activities of Farayand Technique (designated under UNSCR 1737). It manufactures uranium enrichment centrifuge parts, and is directly supporting proliferation sensitive activity that Iran is required to suspend by UNSCRs. Carries out work for Kalaye Electric Company (designated under UNSCR 1737).	26.07.2010
19.	Iran Communications Industries (ICI)	PO Box 19295-4731, Pasdaran Avenue, Tehran, Iran;Alternative address:PO Box 19575-131, 34 Apadana Avenue, Tehran, Iran;Alternative address:Shahid Langary Street, Nobonyad Square Ave, Pasdaran, Tehran	Iran Communications Industries, a subsidiary of Iran Electronics Industries (see no 20), produces various items including communication systems, avionics, optics and electro-optics devices, micro-electronics, information technology, test and measurement, telecommunication security, electronic warfare, radar tube manufacture and refurbishment, and missile launchers. These items can be used in programmes that are under sanction per UNSCR 1737.	26.7.2010
20.	Iran Electronics Industries(including all branches) and subsidiaries:	P. O. Box 18575-365, Tehran, Iran	Wholly-owned subsidiary of MODAFL (and therefore a sister-organisation to AIO, AvIO and DIO). Its role is to manufacture electronic components for Iranian weapons systems.	23.6.2008
	(a)Isfahan Optics	P.O. Box 81465-313 Kaveh Ave. Isfahan - IranP.O. Box 81465-117, Isfahan, Iran	Owned, controlled by, or acts on behalf of Iran Electronics Industries	26.7.2010
	(b)Iran Communications Industries (ICI)	PO Box 19295-4731, Pasdaran Avenue, Tehran, Iran; Alternative address: PO Box 19575-131, 34 Apadana Avenue, Tehran, Iran; Alternative address: Shahid Langary Street, Nobonyad Square Ave, Pasdaran, Tehran	Iran Communications Industries, a subsidiary of Iran Electronics Industries (listed by the EU), produces various items including communication systems, avionics, optics and electro-optics devices, micro-electronics, information technology, test and measurement, telecommunication security, electronic warfare, radar tube manufacture and refurbishment, and missile launchers.	26.7.2010
21.
22.	Iranian Aviation Industries Organization (IAIO)	Ave. Sepahbod Gharani P.O. Box 15815/1775 Tehran, IranAve. Sepahbod Gharani P.O. Box 15815/3446 Tehran, Iran107 Sepahbod Gharani Avenue, Tehran, Iran	A MODAFL (see no 29) organisation responsible for planning and managing Iran's military aviation industry.	26.7.2010
23.	Javedan Mehr Toos		Engineering firm that procures for the Atomic Energy Organisation of Iran which was designated under UNSCR 1737.	26.7.2010
24.	Kala Naft	Kala Naft Tehran Co, P.O. Box 15815/1775, Gharani Avenue, Tehran, Iran;No 242 Shahid Kalantri Street - Near Karim Khan Bridge - Sepahbod Gharani Avenue, Teheran;Kish Free Zone, Trade Center, Kish Island, Iran;Kala Ltd., NIOC House, 4 Victoria Street, London Sw1H1	Trades equipment for oil and gas sector that can be used for Iran's nuclear programme. Attempted to procure material (very hard-wearing alloy gates) which have no use outside the nuclear industry. Has links to companies involved in Iran's nuclear programme.	26.7.2010
25.	Machine Sazi Arak	4th km Tehran Road, PO Box 148, Arak, Iran	Energy sector firm affiliated with IDRO that provides manufacturing support to the nuclear programme, including designated proliferation sensitive activities. Involved in the construction of the Arak heavy-water reactor. UK distributed an export denial notice in July 2009 against Machine Sazi Arak for an 'alumina graphite stopper rod'. In May 2009 Sweden denied the export to Machine Sazi Arak of 'cladding of dish ends for pressure vessels'.	26.7.2010
26.	Marine Industries	Pasdaran Av., PO Box 19585/ 777, Tehran	A subsidiary of the DIO	23.4.2007
27.	Power Plants' Equipment Manufacturing Company (Saakhte Tajhizate Niroogahi)	No. 10, Jahanara Alley, after Hemmat Bridge, Abbaspour St. (previously called Tavanir), Tehran, Post Code 1435733161, Iran	Subordinate to AEOI and Novin Energy (both designated under UNSCR 1737). Involved in the development of nuclear reactors.	26.7.2010
28.	Mechanic Industries Group		Took part in the production of components for the ballistics programme.	23.6.2008
29.	Ministry Of Defense And Support For Armed Forces Logistics (a.k.a. Ministry Of Defense For Armed Forces Logistics; a.k.a. MODAFL; a.k.a. MODSAF)	Located on the west side of Dabestan Street, Abbas Abad District, Tehran, Iran	Responsible for Iran's defence research, development and manufacturing programmes, including support to missile and nuclear programmes.	23.06.2008
30.	Nuclear Fuel Production and Procurement Company (NFPC)	AEOI-NFPD, P.O.Box: 11365-8486, Tehran/IranP.O. Box 14144-1339, Endof North Karegar Ave., Tehran, Iran	Nuclear Fuel Production Division (NFPD) of AEOI runs research and development in the field of nuclear fuel cycle including uranium exploration, mining, milling, conversion and nuclear waste management. The NFPC is the successor to the NFPD, the subsidiary company under the AEOI that runs research and development in the nuclear fuel cycle including conversion and enrichment.	23.4.2007
31.	Parchin Chemical Industries		Worked on propulsion techniques for the Iranian ballistics programme.	23.6.2008
32.	Parto Sanat Co	No. 1281 Valiasr Ave., Next to 14th St., Tehran, 15178 Iran.	Manufacturer of frequency changers and it is capable of developing/modifying imported foreign frequency changers in a way that makes them usable in gas centrifuge enrichment. It is deemed to be involved in nuclear proliferation activities.	26.7.2010
33.	Passive Defense Organization		Responsible for the selection and construction of strategic facilities, including – according to Iranian statements - the uranium enrichment site at Fordow (Qom) built without being declared to the IAEA contrary to Iran's obligations (affirmed in a resolution by the IAEA Board of Governors). Brigadier General Gholam-Reza Jalali, former IRGC is PDO's chairman.	26.7.2010
34.
35.	Raka		A department of Kalaye Electric Company (designated under UNSCR 1737). Established in late 2006, it was responsible for the construction of the Uranium enrichment plant at Fordow (Qom).	26.7.2010
36.	Research Institute of Nuclear Science and Technology a.k.a. Nuclear Science and Technology Research Institute	AEOI, PO Box 14395-836, Tehran	Subordinate to the AEOI and continuing the work of its former Research Division. Its managing director is AEOI Vice President Mohammad Ghannadi (designated in UNSCR 1737).	26.07.2010
37.	Schiller Novin	Gheytariyeh Avenue - no 153 - 3rd Floor - PO BOX 17665/153 6 19389 Teheran	Acting on behalf of Defense Industries Organisation (DIO).	26.7.2010
38.	Shahid Ahmad Kazemi Industrial Group		SAKIG develops and produces surface-to-air missiles systems for Iran's military. It maintains military, missile, and air defense projects and procures goods from Russia, Belarus, and North Korea.	26.7.2010
39.	Shakhese Behbud Sanat		Involved in the production of equipment and parts for the nuclear fuel cycle.	26.7.2010
40.	State Purchasing Organisation (SPO)		The SPO appears to facilitate the import of whole weapons. It appears to be a subsidiary of MODAFL	23.6.2008
41.	Technology Cooperation Office (TCO) of the Iranian President's Office (a.k.a.Center for Innovation and Technology (CITC))	Tehran, Iran	Responsible for Iran's technological advancement through relevant foreign procurement and training links. Supports the nuclear and missile programmes.	26.07.2010
42.	Yasa Part, (including all branches) and subsidiaries:		Company dealing with procurement activities related to the purchase of materials and technologies necessary to nuclear and ballistic programmes.	26.7.2010
	(a)Arfa Paint Company		Acting on behalf of Yasa Part.	26.7.2010
	(b)Arfeh Company		Acting on behalf of Yasa Part.	26.7.2010
	(c)Farasepehr Engineering Company		Acting on behalf of Yasa Part.	26.7.2010
	(d)Hosseini Nejad Trading Co.		Acting on behalf of Yasa Part.	26.7.2010
	(e)Iran Saffron Company or Iransaffron Co.		Acting on behalf of Yasa Part.	26.7.2010
	(f)Shetab G.		Acting on behalf of Yasa Part.	26.7.2010
	(g)Shetab Gaman (a.k.a. Taamin Gostaran Pishgaman Azar)	Address: Norouzi Alley, No 2, Larestan Street, Motahari Avenue, Tehran	Acting on behalf of Yasa Part.	26.7.2010
	(h)Shetab Trading		Acting on behalf of Yasa Part.	26.7.2010
	(i)Y.A.S. Co. Ltd		Acting on behalf of Yasa Part.	26.7.2010
43.	Europäisch-Iranische Handelsbank (EIH)	Head Office: Depenau 2, D-20095 Hamburg; Kish branch, Sanaee Avenue, PO Box 79415/148, Kish Island 79415Tehran branch, No. 1655/1, Valiasr Avenue, PO Box 19656 43 511, Tehran, Iran	EIH has played a key role in assisting a number of Iranian banks with alternative options for completing transactions disrupted by EU sanctions targeting Iran. EIH has been noted acting as the advising bank and intermediary bank in transactions with designated Iranian entities. For example, EIH froze the accounts of EU-designated bank Saderat Iran and Bank Mellat located at EIH Hamburg in early August 2010. Shortly afterwards, EIH resumed Euro-denominated business with Bank Mellat and Bank Saderat Iran using EIH accounts with a non-designated Iranian bank. In August 2010, EIH was setting up a system to enable routine payments to be made to Bank Saderat London and Future Bank Bahrain, in such a way as to avoid EU sanctions.As of October 2010, EIH was continuing to act as a conduit for payments by sanctioned Iranian banks, including Bank Mellat and Bank Saderat. These sanctioned banks are to direct their payments to EIH via Iran's Bank of Industry and Mine. In 2009, EIH was used by Post Bank in a sanctions evasion scheme which involved handling transactions on behalf of UN-designated Bank Sepah. EU-designated Bank Mellat is one of EIH's parent banks.	23.05.2011
44.	Onerbank ZAO (a.k.a. Onerbank ZAT, Eftekhar Bank, Honor Bank, Honorbank, North European Bank)	Ulitsa Klary Tsetkin 51- 1, 220004, Minsk, Belarus	Belarus-based bank owned by Bank Refah Kargaran, Bank Saderat and Bank Toseeh Saderat Iran	23.5.2011
45.	Aras Farayande	Unit 12, No 35 Kooshesh Street, Tehran	Involved in procurement of materials for EU-sanctioned Iran Centrifuge Technology Company	23.05.2011
46.	EMKA Company		A subsidiary company of the UN-sanctioned TAMAS, responsible for the discovery and extraction of uranium.	23.05.2011
47.	Neda Industrial Group	No 10 & 12, 64th Street, Yusef Abad, Tehran	Industrial automation company that has worked for the UN-sanctioned Kalaye Electric Company (KEC) at the uranium fuel enrichment plant at Natanz.	23.05.2011
48.	Neka Novin (a.k.a. Niksa Nirou)	Unit 7, No 12, 13th Street, Mir-Emad St, Motahary Avenue, Tehran, 15875- 6653	Involved in procurement of specialist equipment and materials that have direct application in Iranian nuclear programme.	23.05.2011
49.	Noavaran Pooyamoj (a.k.a. Noavaran Tejarat Paya, Bastan Tejerat Mabna, Behdis Tejarat (or Bazarganis Behdis Tejarat Alborz Company or Behdis Tejarat General Trading Company), Fanavaran Mojpooya, Faramoj Company (or Tosee Danesh Fanavari Faramoj), Green Emirate Paya, Mehbang Sana, Mohandesi Hedayat Control Paya, Pooya Wave Company, Towsee Fanavari Boshra)		Involved in procurement of materials that are controlled and have direct application in the manufacture of centrifuges for Iran's uranium enrichment programme.	23.5.2011
50.	Noor Afza Gostar, (a.k.a. Noor Afzar Gostar)	Opp Seventh Alley, Zarafrshan Street, Eivanak Street, Qods Township	A company that is a subsidiary of the UN-sanctioned Atomic Energy Organisation of Iran (AEOI). Involved in the procurement of equipment for the nuclear programme.	23.05.2011
51.	Pouya Control	No 2, Sharif Alley, Shariati Street, Tehran	A company involved in procurement of inverters for Iran's proscribed enrichment programme.	23.05.2011
52.	Raad Iran (a.k.a Raad Automation Company)	Unit 1, No 35, Bouali Sina Sharghi, Chehel Sotoun Street, Fatemi Square, Tehran	A company involved in procurement of inverters for Iran's proscribed enrichment programme. RaadIran was established to produce and design controlling systems and provides the sale and installation of inverters and programmable Logic Controllers.	23.05.2011
53.	Sureh (a.k.a. Soreh) Nuclear Reactors Fuel Company (a.k.a. Nuclear Fuel Reactor Company; Sookht Atomi Reactorhaye Iran; Soukht Atomi Reactorha-ye Iran)	Head Office: 61 Shahid Abtahi St, Karegar e Shomali, TehranComplex: Persian Gulf Boulevard, Km20 SW Esfahan Road, Esfahan	A company subordinate to the UN-sanctioned Atomic Energy Organisation of Iran (AEOI) consisting of the Uranium Conversion Facility, the Fuel Manufacturing Plant and the Zirconium Production Plant.	23.05.2011
54.	Sun Middle East FZ Company		A company that procures sensitive goods for the Nuclear Reactors Fuel Company (SUREH). Sun Middle East uses intermediaries based outside of Iran to source goods SUREH requires. Sun Middle East provides these intermediaries with false end user details for when the goods are sent to Iran, thereby seeking to circumvent the relevant country's Customs regime.	23.05.2011
55.	Ashtian Tablo	Ashtian Tablo - No 67, Ghods mirheydari St, Yoosefabad, Tehran	Involved in the production and supply of specialist electrical equipment and materials that have a direct application in the Iranian nuclear sector.	23.5.2011
56.	Bals Alman		A manufacturer of electrical equipment (switchgear) involved in the ongoing construction of the Fordow (Qom) facility built without being declared to the IAEA.	23.05.2011
57.	Hirbod Co	Hirbod Co - Flat 2, 3 Second Street, Asad Abadi Avenue, Tehran 14316	A company that has procured goods and equipment destined for Iran's Nuclear and Ballistic Missile programmes for the UN-sanctioned Kalaye Electric Company (KEC).	23.05.2011
58.	Iran Transfo	15 Hakim Azam St, Shirazeh, Shomali St, Mollasadra, Vanak Sq, Tehran	Transformer manufacturer involved in the ongoing construction of the Fordow (Qom) facility built without being declared to the IAEA.	23.05.2011
59.	Marou Sanat (a.k.a. Mohandesi Tarh Va Toseh Maro Sanat Company)	9, Ground Floor, Zohre Street, Mofateh Street, Tehran	Procurement firm that has acted for Mesbah Energy which was designated under UNSCR 1737	23.05.2011
60.	Paya Parto (a.k.a. Paya Partov)		Subsidiary of Novin Energy, which was sanctioned under UNSCR 1747, involved in laser welding.	23.05.2011
61.	Safa Nicu a.k.a. 'Safa Nicu Sepahan', 'Safanco Company', 'Safa Nicu Afghanistan Company', 'Safa Al-Noor Company' and 'Safa Nicu Ltd Company'.	Safa Nicu Building, Danesh Lane, 2nd Moshtagh Street, Esfahan, IranNo 38, Third floor, Molla Sadra Street, Vanak Square, Tehran, IranNo 313, Farvardin Street, Golestan Zone, Ahvaz, IranPO Box 106900, Abu Dhabi, UAENo 233, Lane 15, Vazir Akbar Khan Zone, Kabul, AfghanistanNo 137, First floor, Building No. 16, Jebel Ali, UAE.	Communications firm that supplied equipment for the Fordow (Qom) facility built without being declared to the IAEA.	23.05.2011
62.	Taghtiran		Engineering firm that procures equipment for Iran's IR-40 heavy water research reactor	23.05.2011
63.	Pearl Energy Company Ltd	Level 13(E) Main Office Tower, Jalan Merdeka, Financial Park Complex, Labuan 87000 Malaysia	Pearl Energy Company Ltd. is a wholly- owned subsidiary of First East Export Bank (FEEB), which was designated by the UN under Security Council Resolution 1929 in June 2010. Pearl Energy Company was formed by FEEB in order to provide economic research on an array of global industries.	23.05.2011
64.	Pearl Energy Services, SA	15 Avenue de Montchoisi, Lausanne, 1006 VD, Switzerland; Business Registration Document #CH-550.1.058.055-9	Pearl Energy Services S.A. is a wholly-owned subsidiary of Pearl Energy Company Ltd, located in Switzerland; its mission is to provide financing and expertise to entities seeking to enter in to Iran's petroleum sector.	23.05.2011
65.	West Sun Trade GMBH	Winterhuder Weg 8, Hamburg 22085, Germany;Telephone: 0049 40 2270170; Business Registration Document # HRB45757 (Germany)	Owned or controlled by Machine Sazi Arak	23.05.2011
66.	MAAA Synergy	Malaysia	Involved in procurement of components for Iranian fighter planes	23.05.2011
67.	Modern Technologies FZC (MTFZC)	PO Box 8032, Sharjah, United Arab Emirates	Involved in procurement of components for Iranian nuclear programme	23.05.2011
68.
69.	Bonab Research Center (BRC)	Jade ye Tabriz (km 7), East Azerbaijan, Iran	Affiliated to AEOI	23.05.2011
70.	Tajhiz Sanat Shayan (TSS)	Unit 7, No. 40, Yazdanpanah, Afriqa Blvd., Teheran, Iran	Involved in procurement of components for Iranian nuclear programme	23.05.2011
71.	Institute of Applied Physics (IAP)		Conducts research into military applications of Iranian nuclear programme	23.05.2011
72.	Aran Modern Devices (AMD)		Affiliated to MTFZC network	23.05.2011
73.	Sakhte Turbopomp va Kompressor (SATAK) (a.k.a. Turbo Compressor Manufacturer, TCMFG)	8, Shahin Lane, Tavanir Rd., Valiasr Av., Teheran, Iran	Involved in procurement efforts for Iranian missile programm	23.05.2011
74.	Electronic Components Industries (ECI)	Hossain Abad Avenue, Shiraz, Iran	Subsidiary of Iran Electronics Industries	23.05.2011
75.	Shiraz Electronics Industries	Mirzaie Shirazi, P.O. Box 71365-1589, Shiraz, Iran	Subsidiary of Iran Electronics Industries	23.05.2011
76.	Iran Marine Industrial Company (SADRA)	Sadra Building No 3, Shafagh St., Poonak Khavari Blvd., Shahrak Ghods, P.O. Box 14669-56491, Tehran, Iran	Effectively controlled by Sepanir Oil & Gas Energy Engineering Company, which is designated by the EU as an IRGC company. Provides support to the Government of Iran through its involvement in the Iranian energy sector including in the South Pars Gas field.	23.5.2011
77.	Shahid Beheshti University	Daneshju Blvd., Yaman St., Chamran Blvd., P.O. Box 19839-63113, Tehran, Iran	Shahid Beheshti University is a public entity which is under the supervision of the Ministry of Science, Research and Technology. Carries out scientific research relevant to the development of nuclear weapons.	23.5.2011
78.	Aria Nikan, (a.k.a. Pergas Aria Movalled Ltd)	Suite 1, 59 Azadi Ali North Sohrevardi Avenue, Tehran, 1576935561	Known to procure for EU designated Iran Centrifuge Technology Company (TESA) Commercial Department. They have made efforts to procure designated materials, including goods from the EU, which have applications in the Iranian nuclear programme.	1.12.2011
79.	Bargh Azaraksh; (a.k.a Barghe Azerakhsh Sakht)	No 599, Stage 3, Ata Al Malek Blvd, Emam Khomeini Street, Esfahan.	Company that has been contracted to work at the uranium enrichment sites at Natanz and Qom/Fordow on the electricity and piping works. It was in charge of designing, procuring and installing electrical control equipment at Natanz in 2010.	1.12.2011
80.	Behineh Trading Co	Tehran, Iran	Involved in furnishing ammunition from Iran via Nigeria to a third country	1.12.2011
81.	Eyvaz Technic	No 3, Building 3, Shahid Hamid Sadigh Alley, Shariati Street, Tehran, Iran.	Producer of vacuum equipment that has supplied the uranium enrichment sites at Natanz and Qom/Fordow. In 2011 it supplied pressure transducers to UN-designated Kalaye Electric Company.	1.12.2011
82.	Fatsa	No 84, Street 20, North Amir Abad, Tehran	Iran's Uranium Processing and Nuclear Fuel Production Company. Controlled by the UN-designated Atomic Energy Organisation of Iran.	1.12.2011
83.	Ghani Sazi Uranium Company (a.k.a. Iran Uranium Enrichment Company)	3, Qarqavol Close, 20th Street, Tehran	Subordinate to the UN-designated TAMAS. It has production contracts with UN-designated Kalaye Electric Company and EU-designated TESA.	1.12.2011
84.	Iran Pooya (a.k.a. Iran Pouya)		A government owned company that operated the biggest extruder of aluminium in Iran and supplied material for use in the production of casings for the IR-1 and IR-2 centrifuges. A major manufacturer of aluminium cylinders for centrifuges whose customers include the UN-designated AEOI and EU-designated TESA.	1.12.2011
85.
86.	Karanir (a.k.a. Moaser, a.k.a. Tajhiz Sanat)	1139/1 Unit 104 Gol Building, Gol Alley, North Side of Sae, Vali Asr Avenue. PO Box 19395-6439, Tehran.	Involved in purchasing equipment and materials which have direct applications in the Iranian nuclear programme.	1.12.2011
87.	Khala Afarin Pars	Unit 5, 2nd Floor, No75, Mehran Afrand St, Sattarkhan St, Tehran.	Involved in purchasing equipment and materials which have direct applications in the Iranian nuclear programme.	1.12.2011
88.	MACPAR Makina San Ve Tic	Istasyon MH, Sehitler cad, Guldeniz Sit, Number 79/2, Tuzla 34930, Istanbul	Company run by Milad Jafari who has supplied goods, mostly metals, to UN designated Shahid Hemmat Industries Group (SHIG) through front companies.	1.12.2011
89.	MATSA (Mohandesi Toseh Sokht Atomi Company)	90, Fathi Shaghaghi Street, Tehran, Iran.	Iranian company contracted to UN-designated Kalaye Electric Company to provide design and engineering services across the nuclear fuel cycle. Most recently has been procuring equipment for the Natanz uranium enrichment site.	1.12.2011
90.	Mobin Sanjesh	Entry 3, No 11, 12th Street, Miremad Alley, Abbas Abad, Tehran	Involved in purchasing equipment and materials which have direct applications in the Iranian nuclear programme.	1.12.2011
91.	Multimat lc ve Dis Ticaret Pazarlama Limited Sirketi		Company run by Milad Jafari who has supplied goods, mostly metals, to UN designated Shahid Hemmat Industries Group (SHIG) through front companies.	1.12.2011
92.	Research Centre for Explosion and Impact (a.k.a. METFAZ)	44, 180th Street West, Tehran, 16539-75751	Subordinate to the EU-designated Malek Ashtar University, it oversees activity linked to the Possible Military Dimensions of Iran's nuclear programme upon which Iran is not cooperating with the IAEA.	1.12.2011
93.	Saman Nasb Zayendeh Rood; Saman Nasbzainde Rood	Unit 7, 3rd Floor Mehdi Building, Kahorz Blvd, Esfahan, Iran.	Construction contractor that has installed piping and associated support equipment at the uranium enrichment site at Natanz. It has dealt specifically with centrifuge piping.	1.12.2011
94.	Saman Tose'e Asia (SATA)		Engineering firm involved in supporting a range of large scale industrial projects including Iran's uranium enrichment programme, including undeclared work at the uranium enrichment site at Qom/Fordow.	1.12.2011
95.	Samen Industries	2nd km of Khalaj Road End of Seyyedi St., P.O.Box 91735-549, 91735 Mashhad, Iran, Tel.: +98 511 3853008, +98 511 3870225	Shell name for UN-designated Khorasan Metallurgy Industries, subsidiary of Ammunition Industries Group (AMIG).	1.12.2011
96.	Soreh (Nuclear Fuel Reactor Company)	61 Shahid Abthani Street – Karegar e Shomali, Tehran.; Persian Gulf Boulevard, KM 20 SW, Ispahan	Affiliate of the UN-sanctioned Atomic Energy Organization of Iran (AEOI).	1.12.2011
97.	STEP Standart Teknik Parca San ve TIC A.S.	79/2 Tuzla, 34940, Istanbul, Turkey	Company run by Milad Jafari, who has supplied goods, mostly metals, to UN designated Shahid Hemmat Industrial Group (SHIG) through front companies.	1.12.2011
98.	SURENA (a.k.a. Sakhd Va Rah-An-Da-Zi)		Company for Construction and Commissioning of Nuclear Power Plants. Controlled by the UN designated Novin Energy Company.	1.12.2011
99.	TABA (Iran Cutting Tools Manufacturing company - Taba Towlid Abzar Boreshi Iran)	12 Ferdowsi, Avenue Sakhaee, avenue 30 Tir (sud), nr 66 – Tehran	Owned or controlled by EU-sanctioned TESA, Involved in manufacturing equipment and materials which have direct applications in the Iranian nuclear programme.	1.12.2011
100.	Test Tafsir	No 11, Tawhid 6 Street, Moj Street, Darya Blvd, Shahrak Gharb, Tehran, Iran.	Company produces and has supplied UF6 specific containers to the uranium enrichment sites at Natanz and Qom/Fordow.	1.12.2011
101.	Tosse Silooha (a.k.a. Tosseh Jahad E Silo)		Involved in the Iranian nuclear programme at the Natanz, Qom and Arak facilities.	1.12.2011
102.	Yarsanat (a.k.a. Yar Sanat, a.k.a. Yarestan Vacuumi)	No. 101, West Zardosht Street, 3rd Floor, 14157 Tehran; No. 139 Hoveyzeh Street, 15337, Tehran.	Procurement company for UN-designated Kalaye Electric Company. Involved in purchasing equipment and materials which have direct applications in the Iranian nuclear programme. It has attempted the procurement of vacuum products and pressure transducers.	1.12.2011
103.	Oil Turbo Compressor Company (OTC)	No. 12 Saee Alley Vali E Asr Street, Tehran, Iran	Affiliated to EU-designated Sakhte Turbopomp va Kompressor (SATAK) (a.k.a. Turbo Compressor Manufacturer, TCMFG).	1.12.2011
104.	Central Bank of Iran(a.k.a. Central Bank of the Islamic Republic of Iran)	Postal Address: Mirdamad Blvd., NO. 144,Tehran,Islamic Republic of IranP.O. Box: 15875 / 7177Switchboard: +98 21 299 51Cable Address: MARKAZBANKTelex: 216 219-22 MZBK IR SWIFTAddress: BMJIIRTHWeb Site: http://www.cbi.irE-mail: G.SecDept@cbi.ir	Involved in activities to circumvent sanctions. Provides financial support to the Government of Iran.	23.1.2012
105.	Bank Tejarat	Postal Address: Taleghani Br. 130, Taleghani Ave. P.O. Box: 11365 -5416, Tehran; Tel. 88826690; Tlx.: 226641 TJTA IR; Fax 88893641; Website: http://www.tejaratbank.ir	Bank Tejarat provides significant support to the Government of Iran by offering financial resources and financing services for oil and gas development projects. The oil and gas sector constitutes a significant source of funding for the Government of Iran and several projects financed by Bank Tejarat are carried out by subsidiaries of entities owned and controlled by the Government of Iran. In addition, Bank Tejarat remains partly owned by and closely linked to the Government of Iran which is therefore in a position to influence Bank Tejarat's decisions, including its involvement in the financing of projects regarded by the Iranian Government as a high priority.Furthermore, as Bank Tejarat provides financing to various crude oil productions and refining projects which necessarily require the acquisition of key equipment and technology for those sectors whose supply for use in Iran is prohibited, Bank Tejarat can be identified as being involved in the procurement of prohibited goods and technology.	8.4.2015
106.	Tidewater (a.k.a. Tidewater Middle East Co; Faraz Royal Qeshm Company LLC)	Postal address: No 80, Tidewater Building, Vozara Street, Next to Saie Park, Tehran, Iran	Owned or controlled by IRGC	23.01.2012
107.	Turbine Engineering Manufacturing (TEM) (a.k.a T.E.M. Co.)	Postal address: Shishesh Mina Street, Karaj Special Road, Tehran, Iran	Used as a front company by designated Iran Aircraft Industries (IACI) for covert procurement activities.	23.1.2012
108.	Sad Export Import Company (a.k.a. SAD Import & Export Company)	Postal address: Haftom Tir Square, South Mofte Avenue, Tour Line No; 3/1, Tehran, IranP.O. Box 1584864813 Tehran, Iran	Used as a front company by designated Defence Industries Organization (DIO). Involved in arms transfers to Syria. The company's involvement was also noted in illicit arms transfer aboard M/V Monchegorsk.	23.1.2012
109.	Rosmachin	Postal address: Haftom Tir Square, South Mofte Avenue, Tour Line No; 3/1, Tehran, IranP.O. Box 1584864813 Tehran, Iran	Front company of Sad Export Import Company. Involved in illicit arms transfer aboard M/V Monchgorsk.	23.1.2012
110.	Ministry of Energy	Palestine Avenue North, next to Zarathustra Avenue 81,tel. 9-8901081.	Responsible for policy in the energy sector, which provides a substantial source of revenue for the Iranian Government.	16.10.2012
111.	Ministry of Petroleum	Taleghani Avenue, next to Hafez Bridge,tel. 6214-6153751	Responsible for policy in the oil sector, which provides a substantial source of revenue for the Iranian Government.	16.10.2012
112.	National Iranian Oil Company(NIOC)	NIOC HQ, National Iranian Oil Company Hafez Crossing,Taleghani Avenue Tehran - Iran/First Central Building,Taleghan St., Tehran, Iran,Postal Code: 1593657919P.O. Box 1863 and 2501	State-owned and operated entity providing financial resources to the Government of Iran. The Minister of Oil is Director of the NIOC Board and the Deputy Minister of Oil is the Managing Director of NIOC.	16.10.2012
113.	National Iranian Oil Company(NIOC) PTE LTD	7 Temasek Boulevard #07-02,Suntec Tower One 038987,Singapore;Registration ID 199004388CSingapore	Subsidiary of the National Iranian Oil Company (NIOC).	16.10.2012
114.	National Iranian Oil Company(NIOC)International Affairs Limited	NIOC House,4 Victoria Street,LondonSW1H 0NE,United Kingdom; UKCompany Number 02772297(United Kingdom)	Subsidiary of the National Iranian Oil Company (NIOC).	16.10.2012
115.	Iran Fuel Conservation Organization(IFCO)	No. 23 East Daneshvar St.North Shiraz St.Molasadra St.Vanak Sq.TehranIranTel.: (+98) 2188604760-6	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
116.	Karoon Oil & Gas Production Company	Karoon Industrial ZoneAhwazKhouzestanIranTel.: (+98) 6114446464	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
117.	Petroleum Engineering & Develop-ment Company(PEDEC)	No. 61 Shahid Kalantari St.Sepahbod Qarani Ave.TehranIranTel.: (+98) 2188898650-60	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
118.	North Drilling Company (NDC)	No 8 35th St.Alvand St.Argentine Sq.TehranIranTel. (+ 98) 2188785083-8	North Drilling provides financial support to the Government of Iran through being indirectly owned by the Mostazafan Foundation, a major Iranian parastatal entity controlled by the Government of Iran. North Drilling is an important entity in the energy sector which provides substantial revenues to the Government of Iran. Additionally, North Drilling has imported key equipment for the oil and gas industry, including prohibited goods. Therefore, North Drilling provides support for Iran's proliferation-sensitive nuclear activities.	23.4.2014
119.	Khazar Expl & Prod Co(KEPCO)	No. 19 11th St.Khaled Eslamboli St.TehranIranTel.: (+98) 2188722430	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
120.	National Iranian Drilling Company(NIDC)	Airport Sq.Pasdaran Blvd.AhwazKhouzestanIranTel.: (+98) 6114440151	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
121.	South Zagros Oil & Gas Production Company	Parvaneh St.Karimkhan Zand Blvd.ShirazIranTel.: (+98) 7112138204	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
122.	Maroun Oil & Gas Company	Ahwaz-Mahshahr Rd.(Km 12)AhwazIranTel.: (+98) 6114434073	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
123.	Masjed-soleyman Oil & Gas Company(MOGC)	Masjed SoleymanKhouzestanIranTel.: (+98) 68152228001	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
124.	Gachsaran Oil & Gas Company	GachsaranKohkiluye-va-BoyerAhmadIranTel.: (+98) 7422222581	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
125.	Aghajari Oil & Gas Production Company(AOGPC)	Naft Blvd.OmidiehKhouzestanIranTel.: (+98) 611914701	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
126.	Arvandan Oil & Gas Company(AOGC)	Khamenei Ave.KhoramsharIranTel.: (+98) 6324214021	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
127.	West Oil & Gas Production Company	No. 42 Zan Blvd.Naft Sq.KermanshahIranTel.: (+98) 8318370072	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
128.	East Oil & Gas Production Company(EOGPC)	No. 18 Payam 6 St.Payam Ave.Sheshsad DastgahMashhadIranTel.: (+98) 5117633011	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
129.	Iranian Oil Terminals Company(IOTC)	No. 17 Beyhaghi St.Argentine Sq.TehranIranTel.: (+98) 2188732221	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
130.	Pars Special Economic Energy Zone(PSEEZ)	Pars Special Economic Energy Zone Org.AssaluyehBoushehrIranTel.: (+98) 7727376330	Subsidiary (100 %) of the National Iranian Oil Company (NIOC).	16.10.2012
131.
132.	Naftiran Intertrade Company (a.k.a. Naftiran Trade Company) (NICO)	5th Floor, Petropars Building, No 35 Farhang Boulevard, Snadat Abad Avenue, Tehran, Iran Tel. +98 21 22372486; +98 21 22374681; +98 21 22374678; Fax +98 21 22374678; +98 21 22372481 E-mail: info@naftiran.com	Subsidiary (100 %) of the National Iranian Oil Company (NIOC)	16.10.2012
133.	Naftiran Intertrade Company Srl	Avenue de la Tour-Haldimand, 6, 1009 Pully, SwitzerlandTel: +41 21 3106565Fax: +41 21 3106566/67/72Email: nico.finance@naftiran.ch	Subsidiary (100 %) of the Naftiran Intertrade Company Ltd.	16.10.2012
134.	Petroiran Development Company (PEDCO) Ltd(a.k.a. PetroIran; a.k.a. "PEDCO")	National Iranian Oil Company - PEDCO,P.O. Box 2965,Al Bathaa Tower,9th Floor, Apt. 905, Al Buhaira Corniche, Sharjah,United Arab Emirates;P.O. Box 15875-6731,Tehran,Iran; 41,1st Floor, International House,The Parade,St. Helier JE2 3QQ,Jersey;No. 22, 7th Lane,Khalid Eslamboli Street,Shahid Beheshti Avenue,Tehran,Iran;No. 102, Next to Shahid Amir Soheil Tabrizian Alley,Shahid Dastgerdi (Ex Zafar) Street,Shariati Street,Tehran 19199/45111,Iran;Kish Harbour,Bazargan Ferdos Warehouses,Kish Island,Iran;Registration ID 67493 (Jersey)	Subsidiary of Naftiran Intertrade Company Ltd.	16.10.2012
135.	Petropars Ltd.(a.k.a. Petropasr Limited; a.k.a. "PPL")	Calle La Guairita, Centro Profesional Eurobuilding,Piso 8,Oficina 8E,Chuao,Caracas 1060,Venezuela;No. 35, Farhang Blvd.,Saadat Abad,Tehran,Iran;P.O. Box 3136,Road Town,Tortola,Virgin Islands,British;all offices worldwide.	Subsidiary of Naftiran Intertrade Company Ltd.	16.10.2012
136.	Petropars International FZE(a.k.a. PPI FZE)	P.O. Box 72146,Dubai,United Arab Emirates;all offices worldwide	Subsidiary of Petropars Ltd.	16.10.2012
137.	Petropars UK Limited	47 Queen Anne Street,London W1G 9JG,United Kingdom; UKCompany Number 03503060(United Kingdom);all offices worldwide	Subsidiary of Petropars Ltd.	16.10.2012
138.	National Iranian Gas Company(NIGC)	(1)National Iranian Gas Company Building,South Aban Street,Karimkhan Boulevard,Tehran,Iran(2)P.O. Box 15875,Tehran,Iran(3)NIGC Main Bldg.South Aban St.Karimkhan Ave.,Tehran 1598753113,Iran	State-owned and operated entity that provides financial resources to the Government of Iran. The Minister of Oil is Chairman of NIGC's Board and the Deputy Oil Minister is Managing Director and Vice Chairman of NIGC.	16.10.2012
139.	National Iranian Oil Refining and Distribution Company(NIORDC)	4 Varsho Street,Tehran 1598666611,P.O. Box 15815/3499Tehran	State-owned and operated entity that provides financial support to the Government of Iran. The Minister of Oil is Chairman of NIORDC's Board.	16.10.2012
140.	National Iranian Tanker Company (NITC)	35 East Shahid Atefi Street, Africa Ave., 19177 Tehran, P.O. Box: 19395-4833,Tel: +98 21 23801,Email: info@nitc-tankers.com; all offices worldwide	The National Iranian Tanker Company provides financial support to the Government of Iran through its shareholders the Iranian State Retirement Fund, the Iranian Social Security Organization, and the Oil Industry Employees Retirement and Savings Fund, which are State-controlled entities. Moreover, NITC is one of the largest operators of crude oil carriers in the world and one of the main transporters of Iranian crude oil. Accordingly, NITC provides logistical support to the Government of Iran through the transport of Iranian oil.
141.	Trade Capital Bank	220035 BelarusTimiriazeva str. 65ATel: +375 (17) 3121012Fax +375 (17) 3121008e-mail: info@tcbank.by	Subsidiary (99 %) of Tejarat Bank.	16.10.2012
142.	Bank of Industry and Mine	No. 2817 Firouzeh Tower (above park way junction)Valiaar St.TehranTel. 021-22029859Fax: 021-22260272-5	State owned company which provides financial support to the Government of Iran.	16.10.2012
143.	Cooperative Development Bank(a.k.a. Tose’e Ta’avon Bank)	Bozorgmehr St.Vali-e Asr AveTehranTel: +(9821) 66419974 / 66418184Fax: (+9821) 66419974e-mail: info@sandoghtavon.gov.ir	State owned company which provides financial support to the Government of Iran.	16.10.2012
144.	National Iranian Oil Company Nederland (a.k.a.: NIOC Netherlands Representation Office)	Blaak 512, 3011 TA and Weena 333, 3013 AL Rotterdam, Netherlands.Tel +31 (10) 225 0177, +31 (10) 225 0308.http://www.nioc-intl.com/Offices_Rotterdam.htm.	Subsidiary of the National Iranian Oil Company (NIOC).	7.11.2012
145.	National Iranian Oil Products Distribution Company (NIOPDC)	No.1, Tehran, Iranshahr Ave. Shadab. St,P.O.Box: 79145/3184Tel: +98-21-77606030Website: www.niopdc.ir	Subsidiary of the National Iranian Oil Refining and Distribution Company (NIORDC)	22.12.2012
146.	Iranian Oil Pipelines and Telecommunications Company (IOPTC)	No.194, Tehran, Sepahbod Gharani Ave.Tel: +98-21-88801960/+98-21-66152223Fax: +98-21-66154351Website: www.ioptc.com	Subsidiary of the National Iranian Oil Refining and Distribution Company (NIORDC)	22.12.2012
147.	National Iranian Oil Engineering and Construction Company (NIOEC)	No.263, Tehran, Ostad Nejatollahi Ave.P.O.Box: 11365/6714Tel: +98-21-88907472Fax: +98-21-88907472Website: www.nioec.org	Subsidiary of the National Iranian Oil Refining and Distribution Company (NIORDC)	22.12.2012
148.	Iran Composites Institute	Iran Composites Institute,Iranian University of Science and Technology,16845-188, Tehran, Iran,Telephone: 98 217 3912858Fax: 98 217 7491206E-mail: ici@iust.ac.irWebsite: http://www.irancomposites.org	Iranian Composites Institute (ICI, aka Composite Institute of Iran) is assisting designated entities to violate the provisions of UN and EU sanctions on Iran and is directly supporting Iran's proliferation sensitive nuclear activities. As of 2011 ICI had been contracted to provide EU-designated Iran Centrifuge Technology Company (TESA) with IR-2M centrifuge rotors.	22.12.2012
149.	Jelvesazan Company	22 Bahman St., Bozorgmehr Ave, 84155666, Esfahan, IranTel: 98 0311 2658311 15Fax: 98 0311 2679097	Jelvesazan Company is assisting designated entities to violate the provisions of UN and EU sanctions on Iran and is directly supporting Iran's proliferation sensitive nuclear activities. As of early 2012 Jelvesazan intended to supply controlled vacuum pumps to EU-designated Iran Centrifuge Technology Company (TESA).	22.12.2012
150.
151.	Simatec Development Company		Simatec Development Company is assisting designated entities to violate the provisions of UN and EU sanctions on Iran and is directly supporting Iran's proliferation sensitive nuclear activities. As of early 2010 Simatec was contracted by UN-designated Kalaye Electric Company (KEC) to procure Vacon inverters to power uranium enrichment centrifuges. As of mid-2012 Simatec was attempting to procure EU-controlled inverters.	22.12.2012
152.	Aluminat	1.Parcham St, 13th Km of Qom Rd 38135 Arak (Factory)2.Unit 38, 5th Fl, Bldg No 60, Golfam St, Jordan, 19395-5716, TehranTel: 98 212 2049216 / 22049928 / 22045237Fax: 98 21 22057127Website: www.aluminat.com	Aluminat is assisting designated entities to violate the provisions of UN and EU sanctions on Iran and is directly supporting Iran's proliferation sensitive nuclear activities. In early 2012 Aluminat had a contract to supply 6061-T6 aluminium to EU-designated Iran Centrifuge Technology Company (TESA).	22.12.2012
153.	Organisation of Defensive Innovation and Research (SPND)		The Organisation of Defensive Innovation and Research (SPND) directly supports Iran's proliferation sensitive nuclear activities. The IAEA has identified SPND with their concerns over possible military dimensions (PMD) to Iran's nuclear programme. SPND is run by UN-designated Mohsen Fakhrizadeh-Mahabadi and is part of the Ministry of Defence For Armed Forces Logistics (MODAFL) designated by the EU.	22.12.2012
154.	First Islamic Investment Bank	Branch: 19A-31-3A, Level 31 Business Suite, Wisma UOA, Jalan Pinang 50450, Kuala Lumpur; Kuala Lumpur; Wilayah Persekutuan; 50450 Tel. 603-21620361/2/3/4, +6087417049/417050, +622157948110Branch: Unit 13 (C), Main Office Tower, Financial Park Labuan Complex, Jalan Merdeka, 87000 Federal Territory of Labuan, Malaysia; Labuan F.T; 87000Investor Relations: Menara Prima 17th floor Jalan Lingkar, Mega Kuningan Blok 6.2 Jakarta 12950 — Indonesia; South Jakarta; Jakarta; 12950	First Islamic Investment Bank (FIIB) is providing financial and logistical support to the Government of Iran. FIIB was used by Babak Zanjani to channel a significant amount of Iranian oil-related payments on behalf of the Government of Iran.	22.12.2012
155.	International Safe Oil		International Safe Oil (ISO) is assisting designated entities to violate the provisions of the EU regulation on Iran and is providing financial support to the government of Iran. ISO is part of the Sorinet Group owned and operated by Babak Zanjani. It is being used to channel Iranian oil-related payments.	22.12.2012
156.	Sorinet Commercial Trust Bankers Ltd. (SCT) (a.k.a.: SCT Bankers; SCT Bankers Kish Company (PJS); SCT Bankers Company Branch; Sorinet Commercial Trust)	Sorinet Commercial Trust Bankers, Sadaf Tower, 3rd Floor, Suite No. 301, Kish Island, IranSorinet Commercial Trust Bankers, No.1808, 18th Floor, Grosvenor House Commercial Tower, Sheikh Zayed Road, Dubai, UAE, P.O. Box 31988Tehran branch: Reahi Aiiey, First of Karaj, Maksous Road 9, Tehran, Iran. SWIFT codes: SCERIRTH KSH (Kish Island branch), SCTSAEA1 (Dubai branch), SCERIRTH (Tehran branch)Alternative address for Kish Island branch: Kish Banking Fin Activities Centre, No 42, 4th floor, VC25Alternative addresses for Dubai branch: (1) SCT Bankers Kish Company (PJS), Head Office, Kish Island, Sadaf Tower, 3rd floor, Suite 301, P.O. Box 87. (2) Sheykh Admad, Sheykh Zayed Road, 31988, Dubai, Port, Kish Island.Tels: 09347695504 (Kish Island branch)09347695504/97-143257022-99 (Dubai branch)09347695504 (Tehran branch)Emails: info@sctbankers.comzanjani@sctbankers.com	Sorinet Commercial Trust Bankers Ltd. is controlled by Babak Zanjani, who is designated for providing financial support to the Government of Iran by facilitating oil payments on its behalf.	8.11.2014
157.	HK Intertrade Company Ltd (HK Intertrade)	HK Intertrade Company, 21st Floor, Tai Yau Building, 181 Johnston Road, Wanchai, Hong Kong	HK Intertrade is fully owned and controlled by the National Iranian Oil Company, a designated and state-owned entity that provides support to the Government of Iran. In addition, HK Intertrade has provided logistical and financial support to the Government of Iran by facilitating the transfer of oil-related money on behalf of the Government of Iran.	22.12.2012
158.	Petro Suisse	Petro Suisse Avenue De la Tour- Halimand 6, 1009 Pully, Switzerland	Petro Suisse, a company engaged in the Iranian oil and gas sector, is fully owned by the National Iranian Oil Company (NIOC) which is a designated entity that provides financial support to the Government of Iran. Petro Suisse is also associated with Naftiran Intertrade Co (NICO) which is designated as a subsidiary (100 %) of the National Iranian Oil Company (NIOC).	22.12.2012
159.	Oil industry Pension Fund Investment Company (OPIC)	No 234, Taleghani St, Tehran, Iran	OPIC provides significant support to the Government of Iran by providing financial resources and financing services for oil and gas development projects to a variety of entities linked to the Government of Iran, including subsidiaries of state owned companies (NIOC). Also, OPIC has owned IOEC (Iranian Offshore Engineering Construction Co.) which is EU designated for providing logistical support to the Government of Iran.The oil and gas sector constitutes a significant source of funding for the Government of Iran, and there is a potential connection between Iran's oil revenue derived from its energy sector and the funding of Iran's proliferation sensitive activities.The Managing Director of OPIC is Naser Maleki, who is a United Nations designated individual on the grounds of being Head of the Shahid Hemat Industrial Group (SHIG) and also a MODAFL (Iranian Ministry of Defence and Armed Forces Logistics) official overseeing the work on the Shahab 3 ballistic missile programme (Iran's long range ballistic missile currently in service). SHIG is a United Nations designated entity on the grounds that it is a subordinate entity of Aerospaces Industries Organisation (AIO, which is an EU-designated entity) and involved in Iran's ballistic missile programme. Accordingly, OPIC is directly associated with Iran's proliferation-sensitive nuclear activities or the development of nuclear weapons delivery systems.	1.12.2015
160.	CF Sharp and Company Private Limited		This entity has been assisting the Irano-Hind Shipping Company (IHSC) (designated by the United Nations on 9 June 2010) in circumventing the sanctions adopted against it. Following its designation, IHSC has tried to conceal its ownership of three tankers, by placing them under the management of Noah Ship Management and then Marian Ship Management. CF Sharp and Co. has contributed to this arrangement by concluding a personnel management contract with IHSC covering the crew of those three tankers. That contract was performed by Noah Ship Management and Marian Ship Management.	22.12.2012
161.	Sharif University of Technology	Azadi Ave/Street, PO Box 11365-11155, Tehran, Iran, Tel: +98 21 66 161Email: info@sharif.ir	Sharif University of Technology (SUT) has a number of cooperation agreements with Iranian Government organisations which are designated by the UN and/or the EU and which operate in military or military-related fields, particularly in the field of ballistic missile production and procurement. This includes: an agreement with the EU-designated Aerospace Industries Organisation for inter alia the production of satellites; cooperating with the Iranian Ministry of Defence and the Iranian Revolutionary Guards Corps (IRGC) on smart boat competitions; a broader agreement with the IRGC Air Force which covers developing and strengthening the University's relations, organisational and strategic cooperation;SUT is part of a 6-university agreement which supports the Government of Iran through defence-related research; and SUT teaches graduate courses in unmanned aerial vehicle (UAV) engineering which were designed by the Ministry of Science among others. Taken together, these show a significant record of engagement with the Government of Iran in military or military-related fields that constitutes support to the Government of Iran.	8.11.2014
162.
163.	Petropars Iran Company (aka: PPI)	Address: No. 9,Maaref Street,Farhang Blvd, Saadet Abad,Tehran, Iran.Tel +98-21-22096701- 4.http://www.petropars.com/Subsidiaries/PPI.aspx	Subsidiary of designated entity Petropars Ltd	8.6.2013
164.	Petropars Oilfield Services Company (aka: POSCO)	Address: Kish harbor,PPI Bldg,Tel +98-764-445 03 05,http://www.petropars.com/Subsidiaries/POSCO.aspx.	Subsidiary of designated entity Petropars Iran Company	8.6.2013
165.
166.
167.	Iranian Oil Company (U.K.) Limited (IOC)	Iranian Oil Company (U.K.) Limited, aka IOC.Address: NIOC House 6th Floor,4 Victoria Street,London, United Kingdom,SW1H 0NE	IOC is wholly owned by Naftiran Intertrade Company (NICO). NICO is itself designated under EU sanctions because it is wholly owned by the National Iranian Oil Company (NIOC), which is also an EU designated entity because it provides financial resources to the Governmentof Iran. All three Board Directors of IOC as at 18 December 2012 have previously worked for NIOC in a directorship role, further demonstrating the strong link between IOC and NIOC.	8.6.2013
168.	Post Bank of Iran (a.k.a. Post Bank Iran, Post Bank)	237, Motahari Ave., Tehran, Iran 1587618118Website: www.postbank.ir	Company which is majority owned by the Government of Iran and provides financial support to the Government of Iran.	16.11.2013
169.	Iran Insurance Company (a.k.a. Bimeh Iran)	121 Fatemi Ave., P.O. Box 14155-6363 Tehran, IranP.O. Box 14155-6363, 107 Fatemi Ave., Tehran, Iran	Government-owned company which provides financial support to the Government of Iran.	16.11.2013
170.	Export Development Bank of Iran (EDBI) (including all branches and subsidiaries)	Export Development Building, 21st floor, Tose’e tower, 15th St, Ahmad Qasir Ave, Tehran — Iran, 15138-35711 next to the 15th Alley, Bokharest Street, Argentina Square, Tehran, Iran; Tose’e Tower, corner of 15th St, Ahmad Qasir Ave., Argentine Square, Tehran, Iran; No 129, 21 ‘s Khaled Eslamboli, No 1 Building, Tehran, Iran; C.R. No 86936 (Iran)	Government-owned company which provides financial support to the Government of Iran.	16.11.2013
171.	Persia International Bank Plc	6 Lothbury, London Post Code: EC2R 7HH, United Kingdom	Entity owned by designated entities Bank Mellat and Bank Tejarat.	16.11.2013
172.	Iranian Offshore Engineering & Construction Co. (IOEC)	18 Shahid Dehghani Street, Qarani Street, Tehran 19395-5999Or: No 52 North Kheradmand Avenue (Corner of 6th Alley) Tehran, IRANWeb: http://www.ioec.com/	Important entity in the energy sector which provides substantial revenues to the Government of Iran. As such, IOEC provides financial and logistical support to the Government of Iran.	16.11.2013
173.	Bank Refah Kargaran (a.k.a. Bank Refah)	40, North Shiraz Street, Mollasadra Ave., Vanak Sq., Tehran, Postal Code 19917, IranSwift: REF AIRTH	Entity providing support to the Government of Iran. It is 94 per cent owned by the Iranian Social Security Organisation, which in turn is controlled by the Government of Iran, and it provides banking services to government ministries.	16.11.2013

II.Iranian Revolutionary Guard Corps (IRGC)

A.Persons

	Name	Identifying information	Reasons	Date of listing
1.	IRGC Brigadier-General Javad DARVISH-VAND		Former Deputy Minister and Inspector General of MODAFL.	23.6.2008
2.	Rear Admiral Ali FADAVI		Commander of IRGC Navy	26.7.2010
3.	Parviz FATAH	born 1961	Member of the IRGC. Former Minister of Energy.	26.7.2010
4.	IRGC Brigadier-General Seyyed Mahdi FARAHI		Former head of Iran's Aerospace Industries Organisation (AIO) and former managing director of the UN-designated Defence Industries Organisation (DIO). Member of the IRGC and a Deputy in Iran's Ministry of Defense for Armed Forces Logistics (MODAFL).	23.6.2008
5.	IRGC Brigadier-General Ali HOSEYNITASH		Member of the IRGC. Member of the Supreme National Security Council and involved in formulating policy on nuclear issues.	23.6.2008
6.	IRGC Mohammad Ali JAFARI		Commander of the IRGC	23.6.2008
7.	IRGC Brigadier-General Mostafa Mohammad NAJJAR		Minister for the Interior and former Minister of MODAFL, responsible for all military programmes, including ballistic missiles programmes.	23.6.2008
8.	IRGC Brigadier-General Mohammad Reza NAQDI	Born in 1953, Nadjaf (Iraq)	Deputy Commander of IRGC for Cultural and Social Affairs. Former Commander of Basij Resistance Force.	26.7.2010
9.	BrigGen Mohammad PAKPUR		Commander of IRGC Ground Forces	26.7.2010
10.	Rostam QASEMI (a.k.a. Rostam GHASEMI)	Born in 1961	Former Commander of Khatam al-Anbiya.	26.7.2010
11.	BrigGen Hossein SALAMI		Deputy Commander of the IRGC	26.7.2010
12.	IRGC Brigadier-General Ali SHAMSHIRI		Member of the IRGC. Has held senior roles in MODAFL.	23.6.2008
13.	IRGC Brigadier-General Ahmad VAHIDI		Former Minister of the MODAFL.	23.6.2008
14.	Azim AGHAJANI (also spelled ADHAJANI)		Member of IRGC involved in furnishing ammunition from Iran via Nigeria to a third country	1.12.2011
15.	Abolghassem Mozaffari SHAMS		Former head of Khatam al-Anbiya Construction Headquarters.	1.12.2011
16.	Ali Akbar TABATABAEI (alias Sayed Akbar TAHMAESEBI)		Member of IRGC involved in furnishing ammunition from Iran via Nigeria to a third country	1.12.2011
17.	Ali Ashraf NOURI		IRGC Deputy Commander, IRGC Political Bureau Chief	23.1.2012
18.	Hojatoleslam Ali SAIDI (a.k.a. Hojjat- al-Eslam Ali Saidi or Saeedi		Representative of the Supreme Leader to the IRGC	23.1.2012
19.	IRGC Brigadier-General Amir Ali Haji ZADEH (a.k.a. Amir Ali HAJIZADEH)		IRGC Aerospace Force Commander.	23.1.2012

B.Entities

	Name	Identifying information	Reasons	Date of listing
1.	Iranian Revolutionary Guard Corps (IRGC)	Tehran, Iran	Responsible for Iran's nuclear programme. Has operational control for Iran's ballistic missile programme. Has undertaken procurement attempts to support Iran's ballistic missiles and nuclear programmes	26.7.2010
2.	IRGC Air Force		Operates Iran's inventory of short and medium range ballistic missiles. The head of the IRGC air force was designated by UNSCR 1737 (2006)	23.6.2008
3.	IRGC-Air Force Al-Ghadir Missile Command		The IRGC-Air Force Al-Ghadir Missile Command is a specific element within the IRGC Air Force that has been working with SBIG (designated under UNSCR 1737) with the FATEH 110, short range ballistic missile as well as the Ashura medium range ballistic missile. This command appears to be the entity that actually has the operational control of the missiles.	26.7.2010
4.	Naserin Vahid		Naserin Vahid produces weapons parts on behalf of the IRGC. An IRGC front company.	26.7.2010
5.	IRGC Qods Force	Tehran, Iran	Iran's Iranian Revolutionary Guard Corps (IRGC) Qods Force is responsible for operations outside Iran and is Tehran's principal foreign policy tool for special operations and support to terrorists and Islamic militants abroad. Hizballah used Qods Force-supplied rockets, anti-ship cruise missiles (ASCMs), man-portable air defense systems (MANPADS), and unmanned aerial vehicles (UAVs) in the 2006 conflict with Israel and benefited from Qods Force training on these systems, according to press reporting. According to a varietyof reports, the Qods Force continues to re-supply and train Hizballah on advanced weaponry, anti-aircraft missiles, and long-range rockets. The Qods Force continues to provide limited lethal support, training, and funding to Taliban fighters in southern and western Afghanistan including small arms, ammunition, mortars, and short-range battlefield rockets.Commander has been sanctioned under UNSCR	26.7.2010
6.	Sepanir Oil and Gas Energy Engineering Company (a.k.a. Sepah Nir)		A subsidiary of Khatam al-Anbya Construction Headquarters which was designated under UNSCR 1929. Sepanir Oil and Gas Engineering Company is participating in Iran's South Pars offshore Phase 15-16 gas field development project.	26.7.2010
7.	Bonyad Taavon Sepah (a.k.a. IRGC Cooperative Foundation; Bonyad-e Ta'avon-Sepah; Sepah Cooperative Foundation)	Niayes Highway, Seoul Street, Tehran, Iran	Bonyad Taavon Sepah, also known as the IRGC Cooperative Foundation, was formed by the Commanders of the IRGC to structure the IRGC's investments. It is controlled by the IRGC. Bonyad Taavon Sepah's Board of Trustees is composed of nine members, of whom eight are IRGC members. These officers include the IRGC's Commander in Chief, who is the Chairman of the Board of Trustees, the Supreme Leader's representative to the IRGC, the Basij commander, the IRGC Ground Forces commander, the IRGC Air Force commander, the IRGC Navy commander, the head of the IRGC Information Security Organization, a senior IRGC officer from the Armed Forces General Staff, and a senior IRGC officer from MODAFL.	23.05.2011
8.	Ansar Bank (a.k.a. Ansar Finance and Credit Fund; Ansar Financial and Credit Institute; Ansae Institute; Ansar al-Mojahedin No-Interest Loan Institute; Ansar Saving and Interest Free-Loans Fund)	No. 539, North Pasdaran Avenue, Tehran; Ansar Building, North Khaje Nasir Street, Tehran, Iran	Bonyad Taavon Sepah created Ansar Bank to provide financial and credit services to IRGC personnel. Initially, Ansar Bank operated as a credit union and transitioned in to a fully fledged bank in mid 2009, upon receiving a licence from Iran's Central bank. Ansar Bank, formerly known as Ansar al Mojahedin, has been linked to the IRGC for over 20 years. IRGC members received their salaries through Ansar bank. In addition, Ansar bank provided special benefits to IRGC personnel, includingreduced rates for home furnishings and free, or reduced-cost, health care.	23.05.2011
9.	Mehr Bank (a.k.a Mehr Finance and Credit Institute; Mehr Interest-Free Bank)	No. 182, Shahid Tohidi St, 4th Golsetan, Pasdaran Ave, Tehran 1666943, Iran	Mehr Bank is controlled by Bonyas Taavon Sepah and the IRGC. Mehr Bank provides financial services to the IRGC. According to an open source interview with the head of Bonyad Taavon Sepah, Parviz Fattah (b. 1961), Bonyad Taavon Sepah created Mehr Bank to serve the Basij (paramilitary arm of the IRGC).	23.05.2011
10.	Yas Air	Mehrabad Airport, Tehran	New name for UN and EU sanctioned IRGC Pars Aviation Service Company. In 2011 a Yas Air Cargo Airlines aircraft, travelling from Iran to Syria, inspected in Turkey, was inspected and found to contain conventional arms.	1.12.2011
11.	Behnam Sahriyari Trading Company	Postal address: Ziba Building, 10th Floor, Northern Sohrevardi Street, Tehran, Iran	Involved in the shipment of arms on behalf of the IRGC.	23.1.2012
12.	Etemad Amin Invest Co Mobin	Pasadaran Av. Tehran, Iran	A company owned or controlled by IRGC that contributes to financing the strategic interests of the regime.	26.7.2010

III.Islamic Republic of Iran Shipping Lines (IRISL)

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	Name	Identifying information	Reasons	Date of listing
1.	Mohammad Hossein Dajmar	D.O.B: 19 February 1956.Passport: K13644968 (Iran), expires May 2013.	Chairman and Managing Director of IRISL. He is also Chairman of Soroush Sarzamin Asatir Ship Management Co. (SSA), Safiran Payam Darya Shipping Co. (SAPID), and Hafiz Darya Shipping Co. (HDS), known IRISL affiliates.	23.05.2011
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8.	Gholam Hossein Golparvar	Born on 23 January 1957, Iranian. ID Card No 4207.	Mr Golparvar acts on behalf of IRISL and companies associated with it. He has been commercial director of IRISL, as well as Managing Director and shareholder of the SAPID Shipping Company, non-executive director and shareholder of HDSL, and shareholder of Rhabaran Omid Darya Ship Management Company, which are designated by the EU as acting on behalf of IRISL.
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	Name	Identifying information	Reasons	Date of listing
1.
	k)IRITAL Shipping SRL	Commercial Registry Number: GE 426505 (Italy); Italian Fiscal Code: 03329300101 (Italy); V.A.T. Number: 12869140157 (Italy)Ponte Francesco Morosini 59, 16126 Genova (GE), Italy;	Point of contact for ECL and PCL services. Used by the DIO subsidiary Marine Industries Group (MIG; now known as Marine Industries Organization, MIO) which is responsible for the design and construction of various marine structures and both military and non- military vessels. DIO was designated under UNSCR 1737.	26.7.2010
2.	Darya Capital Administration GMBH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB94311 (Germany) issued 21 Jul 2005Schottweg 6, 22087 Hamburg, Germany;Business Registration No. HRB96253, issued Jan 30, 2006	Darya Capital Administration is a wholly owned subsidiary of IRISL Europe GmbH. Its Managing Director is Mohammad Talai.	23.05.2011
3.	Nari Shipping and Chartering GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany;Business Registration Document # HRA102485 (Germany) issued 19 Aug 2005;Telephone: 004940278740	Owned by Ocean Capital Administration and IRISL Europe. Ahmad Sarkandi is also the director of Ocean Capital Administration GmbH and Nari Shipping and Chartering GmbH & Co. KG.	23.05.2011
4.	Ocean Capital Administration GmbH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB92501 (Germany) issued 4 Jan 2005	A German-based IRISL holding company that is owned and controlled by IRISL.	8.4.2015
5.	First Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB94311 (Germany) issued 21 Jul 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
5a.	First Ocean GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRA102601 (Germany) issued 19 Sep 2005; IMO Nr. 9349576	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
6.	Second Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB94312 (Germany) issued 21 Jul 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
6a.	Second Ocean GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRA102502 (Germany) issued 24 Aug 2005; IMO Nr.: 9349588.	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
7.	Third Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB94313 (Germany) issued 21 Jul 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
7a.	Third Ocean GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRA102520 (Germany) issued 29 Aug 2005; IMO Nr.:9349590	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
8.	Fourth Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB94314 (Germany) issued 21 Jul 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
8a.	Fourth Ocean GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRA102600 (Germany) issued 19 Sep 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
9.	Fifth Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB94315 (Germany) issued 21 Jul 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
9a.	Fifth Ocean GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRA102599 (Germany) issued 19 Sep 2005; IMO Nr.: 9349667	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
10.	Sixth Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB94316 (Germany) issued 21 Jul 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
10a.	Sixth Ocean GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRA102501 (Germany) issued 24 Aug 2005; IMO Nr.: 9349679	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
11.	Seventh Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB94829 (Germany) issued 19 Sep 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
11a.	Seventh Ocean GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRA102655 (Germany) issued 26 Sep 2005; IMO Nr.: 9165786	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
12.	Eighth Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB94633 (Germany) issued 24 Aug 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
12a.	Eighth Ocean GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRA102533 (Germany) issued 1 Sep 2005; IMO Nr.: 9165803	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
13.	Ninth Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB94698 (Germany) issued 9 Sep 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
13a.	Ninth Ocean GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRA102565 (Germany) issued 15 Sep 2005; IMO Nr.: 9165798	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
14.	Tenth Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
14a.	Tenth Ocean GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRA102679 (Germany) issued 27 Sep 2005; IMO Nr.: 9165815	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
15.	Eleventh Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB94632 (Germany) issued 24 Aug 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
15a.	Eleventh Ocean GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRA102544 (Germany) issued 9 Sep 2005; IMO Nr. 9209324	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
16.	Twelfth Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRB94573 (Germany) issued 18 Aug 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
16a.	Twelfth Ocean GmbH & Co. KG	Schottweg 5, Hamburg 22087, Germany; Business Registration Document # HRA102506 (Germany) issued 25 Aug 2005	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
17.	Thirteenth Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
17.a.	Thirteenth Ocean GmbH & CO. KG	Schottweg 5, Hamburg 22087, Germany;c/o Islamic Republic of Iran Shipping Lines (IRISL), No. 37, Aseman Tower, Sayyade Shirazee Square, Pasdaran Ave., P.O. Box 19395-1311, Tehran, Iran;Business Registration Document # HRA104149 (Germany) issued 10 Jul 2006;Email Address smd@irisl.net;Website www.irisl.net;Telephone: 00982120100488;Fax: 00982120100486IMO Nr.: 9328900	Owned or controlled by IRISL	23.05.2011
18.	Fourteenth Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
18.a.	Fourteenth Ocean GmbH & CO. KG	Schottweg 5, Hamburg 22087, Germany;c/o Islamic Republic of Iran Shipping Lines (IRISL), No. 37, Aseman Tower, Sayyade Shirazee Square, Pasdaran Ave., P.O. Box 19395-1311, Tehran, Iran;Business Registration Document # HRA104174 (Germany) issued 12 Jul 2006;Email Address smd@irisl.net;Website www.irisl.net;Telephone: 00982120100488;Fax: 00982120100486	Owned or controlled by IRISL	23.05.2011
19.	Fifteenth Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
19.a.	Fifteenth Ocean GmbH & CO. KG	Schottweg 5, Hamburg 22087, Germany;c/o Islamic Republic of Iran Shipping Lines (IRISL), No. 37, Aseman Tower, Sayyade Shirazee Square, Pasdaran Ave., P.O. Box 19395-1311, Tehran, Iran;Business Registration Document # HRA104175 (Germany) issued 12 Jul 2006;Email Address smd@irisl.net;Website www.irisl.net;Telephone: 00982120100488;Fax: 00982120100486IMO Nr.: 9346536	Owned or controlled by IRISL	23.05.2011
20.	Sixteenth Ocean Administration GmbH	Schottweg 5, Hamburg 22087, Germany	Owned by IRISL through Ocean Capital Administration GmbH which is an IRISL holding company.	8.4.2015
20.a.	Sixteenth Ocean GmbH & CO. KG	Schottweg 5, Hamburg 22087, Germany;c/o Islamic Republic of Iran Shipping Lines (IRISL), No. 37, Aseman Tower, Sayyade Shirazee Square, Pasdaran Ave., P.O. Box 19395-1311, Tehran, Iran;Email Address smd@irisl.net;Website www.irisl.net;Telephone: 00982120100488;Fax: 00982120100486	Owned or controlled by IRISL	23.05.2011
21.	Loweswater Ltd	Manning House, 21 Bucks Road, Douglas, Isle of Man, IM1 3DA	Isle of Man-administered company that controls ship-owning companies in Hong Kong. The ships are operated by EU-sanctioned Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned by IRISL. The Hong Kong companies are: Insight World Ltd, Kingdom New Ltd, Logistic Smart Ltd, Neuman Ltd and New Desire Ltd. Technical management of the vessels is carried out by EU-sanctioned Soroush Saramin Asatir (SSA).	23.05.2011
21.a.	Insight World Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nrs.: 8309634; 9165827	Insight World Ltd is a Hong Kong based company, owned by Loweswater Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
21.b.	Kingdom New Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nrs.: 8309622; 9165839	Kingdom New Ltd is a Hong Kong based company, owned by Loweswater Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
21.c.	Logistic Smart Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO nr.: 9209336	Logistic Smart Ltd is a Hong Kong based company, owned by Loweswater Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
21.d.	Neuman Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nrs.: 8309646; 9167253	Neuman Ltd is a Hong Kong based company, owned by Loweswater Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
21.e.	New Desire LTD	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nrs.: 8320183; 9167277	New Desire LTD is a Hong Kong based company, owned by Loweswater Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
22.	Mill Dene Ltd	Manning House, 21 Bucks Road, Douglas, Isle of Man. IM1 3DA	Isle of Man-administered company that controls ship-owning companies in Hong Kong. The ships are operated by EU-sanctioned Safiran Payma Darya Shipping lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned by IRISL. One shareholder is Gholamhossein Golpavar, managing director of SAPID shipping IRISL's commercial director. The Hong Kong Companies are: Advance Novel, Alpha Effort Ltd, Best Precise Ltd, Concept Giant Ltd and Great Method Ltd. Technical management of the vessels is carried out by EU-sanctioned Soroush Saramin Asatir (SSA).	23.05.2011
22.a.	Advance Novel	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nr.: 8320195	Advance Novel is a Hong Kong based company, owned by Mill Dene Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
22.b.	Alpha Effort Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nr. 8309608	Alpha Effort Ltd is a Hong Kong based company, owned by Mill Dene Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
22.c.	Best Precise Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nrs.: 8309593; 9051650	Best Precise Ltd is a Hong Kong based company, owned by Mill Dene Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
22.d.	Concept Giant Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nrs.: 8309658; 9051648	Concept Giant Ltd is a Hong Kong based company, owned by Mill Dene Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
22.e.	Great Method Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nrs.: 8309610; 9051636	Great Method Ltd is a Hong Kong based company, owned by Mill Dene Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
23.	Shallon Ltd	Manning House, 21 Bucks Road, Douglas, Isle of Man. IM1 3DA	Isle of Man-administered company that controls ship-owning companies in Hong Kong. The ships are operated by EU-sanctioned Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned by IRISL. One shareholder is Mohammed Mehdi Rasekh, an IRISL board member. The Hong Kong companies are Smart Day Holdings Ltd, System Wise Ltd (AKA Sysyem Wise Ltd), Trade Treasure, TrueHonour Holdings Ltd. Technical management of the vessels is carried out by EU-sanctioned Soroush Saramin Asatir (SSA).	23.05.2011
23.a.	Smart Day Holdings Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nr. 8309701	Smart Day Holdings Ltd is a Hong Kong based company, owned by Shallon Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
23.b.	System Wise Ltd (a.k.a Sysyem Wise Ltd)	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong Kong	System Wise Ltd is a Hong Kong based company, owned by Shallon Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
23.c.	Trade Treasure	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nr.: 8320157	Trade Treasure is a Hong Kong based company, owned by Shallon Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL	23.05.2011
23.d.	True Honour Holdings Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nr.: 8320171	True Honour Holdings Ltd is a Hong Kong based company, owned by Shallon Ltd, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL	23.05.2011
24.	Springthorpe Limited	Manning House, 21 Bucks Road, Douglas, Isle of Man, IM1 3DA	Isle of Man-administered company that controls ship-owning companies in Hong Kong. The ships are operated by Safiran Payam Darya Shipping Lines (SAPID) which took over IRISL's bulk services and routes and uses vessels previously owned by IRISL. One shareholder is Mohammed Hossein Dajmar, the managing director of IRISL. The Hong Kong companies are: New Synergy Ltd, Partner Century Ltd, Sackville Holdings Ltd, Sanford Group and Sino Access Holdings. Technical Management of the vessels is carried out by EU-sanctioned Soroush Saramin Asatir (SSA).	23.05.2011
24.a.	New Synergy Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nrs.: 8309696; 9167291	New Synergy Ltd is a Hong Kong based company, owned by Springthorpe Limited, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
24.b.	Partner Century Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nr.: 8309684	Partner Century Ltd is a Hong Kong based company, owned by Springthorpe Limited, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
24.c.	Sackville Holdings Ltd	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nrs.: 8320169; 9167265	Sackville Holdings Ltd is a Hong Kong based company, owned by Springthorpe Limited, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
24.d.	Sanford Group	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong Kong	Sanford Group is a Hong Kong based company, owned by Springthorpe Limited, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
24.e.	Sino Access Holdings	15th Floor, Tower One, Lippo Centre, 89 Queensway, Hong KongIMO Nr.: 8309672	Sino Access Holdings is a Hong Kong based company, owned by Springthorpe Limited, whose ships are operated by Safiran Payam Darya Shipping Lines (SAPID) that took over IRISL's bulk services and routes and uses vessels previously owned and operated by IRISL.	23.05.2011
25.
26.
26.a.
26.b.
26.c.
26.d.
27.
28.	Ashtead Shipping Company Ltd	Business registration #108116C,Manning House, 21 Bucks Road, Douglas, IM1 3DA, Isle of Man	Ashtead Shipping Company Ltd is an IRISL front company located in the Isle of Man. It is 100 percent owned by IRISL and is the registered owner of a vessel owned by IRISL or an IRISL affiliate. Ahmad Sarkandi is a director of the company.	23.05.2011
29.	Byfleet Shipping Company Ltd	Byfleet Shipping Company Ltd - Business Registration #118117C, Manning House, 21 Bucks Road, Douglas, IM1 3DA, Isle of Man	Byfleet Shipping Company Ltd is an IRISL front company located in the Isle of Man. It is 100 percent owned by IRISL and is the registered owner of a vessel owned by IRISL or an IRISL affiliate. Ahmad Sarkandi is a director of the company.	23.05.2011
30.	Cobham Shipping Company Ltd	Business Registration #108118C,Manning House, 21 Bucks Road, Douglas, IM1 3DA, Isle of Man	Cobham Shipping Company Ltd is an IRISL front company located in the Isle of Man. It is 100 percent owned by IRISL and is the registered owner of a vessel owned by IRISL or an IRISL affiliate. Ahmad Sarkandi is a director of the company.	23.05.2011
31.	Dorking Shipping Company Ltd	Manning House, 21 Bucks Road, Douglas, IM1 3DA, Isle of ManBusiness Registration #108119C	Dorking Shipping Company Ltd is an IRISL front company located in the Isle of Man. It is 100 percent owned by IRISL and is the registered owner of a vessel owned by IRISL or an IRISL affiliate. Ahmad Sarkandi is a director of the company.	23.05.2011
32.	Effingham Shipping Company Ltd	Manning House, 21 Bucks Road, Douglas, IM1 3DA, Isle of ManBusiness Registration #108120C	Effingham Shipping Company Ltd is an IRISL front company located in the Isle of Man. It is 100 percent owned by IRISL and is the registered owner of a vessel owned by IRISL or an IRISL affiliate. Ahmad Sarkandi is a director of the company.	23.05.2011
33.	Farnham Shipping Company Ltd	Manning House, 21 Bucks Road, Douglas, IM1 3DA, Isle of ManBusiness Registration #108146C	Farnham Shipping Company Ltd is an IRISL front company located in the Isle of Man. It is 100 percent owned by IRISL and is the registered owner of a vessel owned by IRISL or an IRISL affiliate. Ahmad Sarkandi is a director of the company.	23.05.2011
34.	Gomshall Shipping Company Ltd	Manning House, 21 Bucks Road, Douglas, IM1 3DA, Isle of ManBusiness Registration #111998C	Gomshall Shipping Company Ltd is an IRISL front company located in the Isle of Man. It is 100 percent owned by IRISL and is the registered owner of a vessel owned by IRISL or an IRISL affiliate. Ahmad Sarkandi is a director of the company.	23.05.2011
35.	Horsham Shipping Company Ltd	Manning House, 21 Bucks Road, Douglas, IM1 3DA, Isle of ManHorsham Shipping Company Ltd - Business Registration #111999CIMO Nr.: 9323833	Horsham Shipping Company Ltd is an IRISL front company located in the Isle of Man. It is 100 percent owned by IRISL and is the registered owner of a vessel owned by IRISL or an IRISL affiliate. Ahmad Sarkandi is a director of the company.	23.05.2011
36.	E-Sail a.k.a.E-Sail Shipping Company a.k.a. Rice Shipping	Suite 1501, Shanghai Zhong Rong Plaza, 1088 Pudong South Road, Shanghai, China	New names for EU-sanctioned Sant ex Lines, alias IRISL China Shipping Company Limited. Acts on behalf of IRISL. Acts on behalf of EU-designated SAPID in China, chartering IRISL vessels to other firms.	1.12.2011
37.	IRISL Maritime Training Institute	No 115, Ghaem Magham Farahani St. P.O. Box 15896-53313, Tehran, Iran	IRISL Maritime Training Institute is owned and controlled by IRISL which holds 90 % of the company's shares and whose representative is Vice-President of the Board of Directors. It is involved in the training of IRISL employees.	8.4.2015
38.	Kara Shipping and Chartering Gmbh (KSC)	Schottweg 7, 22087 Hamburg, Germany.	Front company for EU-sanctioned HTTS.	1.12.2011
39.	Kheibar Co.	Iranshahr shomali (North) avenue, nr 237, 158478311 Tehran, Iran	Kheibar Co. is owned and controlled by IRISL which holds 81 % of the company's shares and whose representative is a member of its Board of Directors. It provides spare parts for shipping vessels.	8.4.2015
40.	Kish Shipping Line Manning Co.	Sanaei Street Kish Island Iran	Kish Shipping Line Manning Co. is owned and controlled by IRISL. It is involved in the recruitment and personnel management of IRISL.	8.4.2015
41.	Boustead Shipping Agencies Sdn Bhd	Suite P1.01, Level 1 Menara Trend, Intan Millennium Square, 68, Jalan Batai Laut 4, Taman Intan, 41300 Klang, Selangor, Malaysia	Company acting on behalf of IRISL. Boustead Shipping Agencies handles transactions initiated by IRISL by entities owned or controlled by IRISL.	1.12.2011
42.	Diamond Shipping Services (DSS)	5 Saint Catharine Sq., El Mansheya El Soghra, Alexandria, Egypt	Company acting on behalf of IRISL. Diamond Shipping Services handled and profited from transactions initiated by IRISL or entities owned or controlled by IRISL.	1.12.2011
43.
44.	Ocean Express Agencies Private Limited	Ocean Express Agencies - Ground Floor, KDLB Building, 58 West Wharf Road - Karachi - 74000, Sindh, Pakistan	Company acting on behalf of IRISL. Ocean Express Agencies Private Limited used IRISL transport documents and documents used by entities owned or controlled by IRISL to circumvent sanctions.	1.12.2011
45.	OTS Steinweg Agency	Steinweg - OTS, Iskele Meydani, Alb. Faik Sozdener Cad., No:11 D:8 Kat:4 Kadikoy - 34710 Istanbul	Company acting on behalf of IRISL. OTS Steinweg Agency handled transactions for IRISL et entities owned or controlled by IRISL, was involved in setting up front companies owned or controlled by IRISL, involved in acquiring vessels on behalf of IRISL or entities owned or controlled by IRISL.	1.12.2011
46.	Universal Transportation Limitation Utl	21/30 Thai Wah Tower 1, South Sathorn Road, Bangkok 10120 Thailand	Company acting on behalf of IRISL. Universal Transportation Limited (UTL) issued false transport document in the name of a front company owned or controlled by IRISL, handled transactions on behalf of IRISL.	1.12.2011
47.	Walship SA	Cité Les Sources 400 logts, Promotion, Sikh cage B no3 - 16005 Bir Mourad Rais, Algeria	Company acting on behalf of IRISL. Walship SA handled transactions on behalf of IRISL for the benefit of its clients, issued transport documents and invoices in the name of an IRISL front company, sought out potential clients to operate routes in their own name but for the sole benefit of entities owned or controlled by IRISL.	1.12.2011
48.	Acena Shipping Company Limited	Address: 284 Makarios III avenue, Fortuna Court, 3105 LimassolIMO Nrs.: 9213399; 9193185	Acena Shipping Company Limited is a front company owned or controlled by IRISL. It is the registered owner of several vessels owned by IRISL or an IRISL affiliate.	1.12.2011
49.	Alpha Kara Navigation Limited	171, Old Bakery Street, Valetta – Registration number C 39359	Alpha Kara Navigation Limited is a front company owned or controlled by IRISL. Subsidiary of EU-designated Darya Capital Administration GMBH. It is the registered owner of several vessels owned by IRISL or an IRISL affiliate.	1.12.2011
50.	Alpha Nari Navigation Limited	143 Tower Road - 1604 Sliema, Malta Registration number C 38079	Alpha Nari Navigation Limited is a front company owned or controlled by IRISL. It is the registered owner of several vessels owned by IRISL or an IRISL affiliate.	1.12.2011
51.	Aspasis Marine Corporation	Address: 107 Falcon House, Dubai Investment Park, Po Box 361025 Dubai	Aspasis Marine Corporation is a front company owned or controlled by IRISL. It is the registered owner of several vessels owned by IRISL or an IRISL affiliate.	1.12.2011
52.	Atlantic Intermodal		Owned by IRISL agent Pacific Shipping. Rendered financial assistance for impounded IRISL vessels and acquisition of new shipping containers.	1.12.2011
53.	Avrasya Container Shipping Lines		IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
54.	Azores Shipping Company alias Azores Shipping FZE LLC	P.O. Box 113740 – Office no 236,Sultan Business Center,Oud Mehta,Dubai, UAE	Controlled by Mohammad Moghddami Fard. Provides services for the IRISL subsidiary, EU-designated Valfajre Shipping Company. Front company owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned or controlled by IRISL. Moghddami Fard is a company director.	1.12.2011
55.	Beta Kara Navigation Ltd	Address: 171, Old Bakery Street, ValettaRegistration number C 39354	Beta Kara Navigation Ltd is a front company owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of several vessels owned by IRISL or an IRISL affiliate.	1.12.2011
56.	Bis Maritime Limited	Numéro IMO: 0099501	Bis Maritime Limited is an IRISL front company located in Barbados. It is the registered owner of a vessel owned or controlled by IRISL or an IRISL affiliate. Gholam Hossein Golparvar is a company director.	1.12.2011
57.	Brait Holding SA	registered in the Marshall Islands in August 2011 under the number 46270.	IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
58.	Bright Jyoti Shipping		IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
59.	Bright Ship FZC	Saif zone, Dubai	IRISL front company, used to acquire a vessel owned by IRISL or an IRISL affiliate and to transfer funds to IRISL.	1.12.2011
60.	Bright-Nord GmbH und Co. KG	Kattrepelsbrücke 1, 20095 Hamburg, Germany	Owned or controlled by or acting on behalf of IRISL	1.12.2011
61.	CF Sharp Shipping Agencies Pte Ltd	15 New Bridge Road, Rocha House, Singapore 059385	IRISL front company, owned or controlled by IRISL	1.12.2011
62.	Chaplet Shipping Limited	Dieudonnee No1., Triq Tumas Fenech, Qormi, 19635-1114 Malta	IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
63.	Cosy-East GmbH und Co. KG	Kattrepelsbrücke 1, 20095 Hamburg, Germany	Owned or controlled by or acting on behalf of IRISL	1.12.2011
64.	Crystal Shipping FZE	Dubai, UAE	Owned by IRISL agent Pacific Shipping. Set up in 2010 by Moghddami Fard as part of efforts to circumvent EU designation of IRISL. In December 2010 it was used to transfer funds to release impounded IRISL ships and to mask IRISL involvement.	1.12.2011
65.	Damalis Marine Corporation		IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
66.	Delta Kara Navigation Ltd	171, Old Bakery Street, ValettaRegistration number C 39357	IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
67.	Delta Nari Navigation Ltd	143 Tower Road - 1604 Sliema, MaltaRegistration number C 38077	IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
68.	Elbrus Ltd	Manning House - 21 Bucks Road - Douglas - Isle of Man - IM1 3DA	Holding company owned or controlled by IRISL covering a group of IRISL front companies located in the Isle of Man.	1.12.2011
69.	Elcho Holding Ltd	registered in the Marshall Islands in August 2011 under number 46041.	IRISL front company registered in the Marshall Islands, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
70.	Elegant Target Development Limited	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8320195	Owned or controlled by or acting on behalf of IRISL. IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
71.	Epsilon Nari Navigation Ltd	143 Tower Road - 1604 Sliema, MaltaRegistration number C 38082	IRISL front company owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
72.	Eta Nari Navigation Ltd	171, Old Bakery Street, ValettaRegistration number C 38067	IRISL front company owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
73.	Eternal Expert Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong Kong	IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
74.	Fairway Shipping	83 Victoria Street, London, SW1H OHW	IRISL front company owned or controlled by IRISL or an IRISL affiliate. Haji Pajand is a director of Fairway Shipping	1.12.2011
75.	Fasirus Marine Corporation		IRISL front company in Barbados. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
76.	Galliot Maritime Incorporation		IRISL front company in Barbados. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
77.	Gamma Kara Navigation Ltd	171, Old Bakery Street, ValettaRegistration number C 39355	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
78.	Giant King Limited	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8309593	Owned or controlled by or acting on behalf of IRISL.IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
79.	Golden Charter Development Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8309610	Owned or controlled by or acting on behalf of IRISLIRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
80.	Golden Summit Investments Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8309622	Owned or controlled by or acting on behalf of IRISLIRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
81.	Golden Wagon Development Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO Nr.: 8309634	Owned or controlled by or acting on behalf of IRISLIRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
82.	Grand Trinity Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8309658	Owned or controlled by or acting on behalf of IRISLIRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
83.	Great Equity Investments Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8320121	Owned or controlled by or acting on behalf of IRISLIRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
84.	Great Ocean Shipping Services (GOSS)	Suite 404, 4th Floor, Block B-1 PO Box 3671, Ajman FreeTrade Zone, Ajman, UAE	This firm was used to set up cover companies for IRISL in the UAE, including Good Luck Shipping. Its managing director is Moghddami Fard.	1.12.2011
85.	Great Prospect International Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8309646	Owned or controlled by or acting on behalf of IRISLIRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
86.	Great-West GmbH und Co. KG	Kattrepelsbrücke 1, 20095 Hamburg, Germany	Owned or controlled by or acting on behalf of IRISL	1.12.2011
87.	Happy-Süd GmbH und Co. KG	Kattrepelsbrücke 1, 20095 Hamburg, Germany	Owned or controlled by or acting on behalf of IRISL	1.12.2011
88.	Harvest Supreme Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8320183	Owned or controlled by or acting on behalf of IRISLIRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
89.	Harzaru Shipping	IMO number of the vessel: 7027899	IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
90.	Heliotrope Shipping Limited	Dieudonnee No1., Triq Tumas Fenech, Qormi, 19635-1114 Malta – Registration number C 45613IMO number of the vessel: 9270646	IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
91.	Helix Shipping Limited	Dieudonnee No1., Triq Tumas Fenech, Qormi, 19635-1114 Malta – Registration number C 45618IMO number of the vessel: 9346548	IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
92.	Hong Tu Logistics Private Limited	149 Rochor Road 01 - 26 Fu Lu Shou Complex, Singapore 188425	IRISL front company. Owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
93.	Ifold Shipping Company Limited	Dieudonnee No1., Triq Tumas Fenech, Qormi, 19635-1114 Malta – Registration number C 38190IMO Nr.: 9386500	IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
94.	Indus Maritime Incorporation	47st Bella Vista and Aquilino de la Guardia, Panama City, PanamaIMO Nr.: 9283007	IRISL front company in Panama. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
95.	Iota Nari Navigation Limited	143 Tower Road - 1604 Sliema, MaltaRegistration number C 38076	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
96.	ISIM Amin Limited	147/1 Ste Lucia Street, 1185, Valetta - Registration number C 40069	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
97.	Isim Atr Limited	147/1 Ste Lucia Street, 1185, Valetta - Registration number C 34477	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
98.	Isim Olive Limited	147/1 Ste Lucia Street, 1185, Valetta - Registration number C 34479	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
99.	Isim Sat Limited	147/1 Ste Lucia Street, 1185, Valetta - Registration number C 34476	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
100.	ISIM Sea Chariot Ltd	147/1 Ste Lucia Street, 1185, Valetta - Registration number C 45153	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
101.	ISIM Sea Crescent Ltd	147/1 Ste Lucia Street, 1185, Valetta - Registration number C 45152	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
102.	ISIM Sinin Limited	147/1 Ste Lucia Street, 1185, Valetta - Registration number C 41660	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
103.	ISIM Taj Mahal Ltd	147/1 Ste Lucia Street, 1185, Valetta - Registration number C 37437IMO number of the vessel: 9274941	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
104.	Isim Tour Company Limited	147/1 Ste Lucia Street, 1185, Valetta - Registration number C 34478IMO number of the vessel: 9364112	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
105.	Jackman Shipping Company	Dieudonnee No 1., Triq Tumas Fenech, Qormi, 19635-1114 Malta - No C 38183IMO number of the vessel; 9387786	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
106.	Kalan Kish Shipping Company Ltd		IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
107.	Kappa Nari Navigation Ltd	143 Tower Road - 1604 Sliema, MaltaRegistration number C 38066.	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
108.	Kaveri Maritime Incorporation	PanamaRegistration number 5586832IMO Nr.: 9284154	IRISL front company in Panama, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
109.	Kaveri Shipping Llc		IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
110.	Key Charter Development Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong Kong	Owned or controlled by or acting on behalf of IRISL	1.12.2011
111.	King Prosper Investments Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8320169	Owned or controlled by or acting on behalf of IRISLIRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
112.	Kingswood Shipping Company Limited	171, Old Bakery Street, ValettaIMO Nr.: 9387798	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
113.	Lambda Nari Navigation Limited	143 Tower Road - 1604 Sliema, MaltaRegistration number C 38064	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
114.	Lancing Shipping Company limited	Address: 143/1 Tower Road, Sliema - No C 38181IMO number of the vessel: 9387803	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
115.	Magna Carta Limited		IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
116.	Malship Shipping Agency	Registration number C 43447.	IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
117.	Master Supreme International Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8320133	Owned or controlled by or acting on behalf of IRISLIRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
118.	Melodious Maritime Incorporation	47st Bella Vista and Aquilino de la Guardia, Panama City, PanamaIMO number: 9284142	IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
119.	Metro Supreme International Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8309672	Owned or controlled by or acting on behalf of IRISLIRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
120.	Midhurst Shipping Company Limited (Malta)	Special Purpose Company owned by Hassan Djalilzaden – Registration number C38182IMO number of the vessel: 9387815	IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
121.	Modality Ltd	No: C 49549	IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
122.	Modern Elegant Development Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8309701	Owned or controlled by or acting on behalf of IRISLIRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
123.	Morison Menon Chartered Accountant	204 Tower A2, Gulf Towers, Dubai, PoBox 5562 et 8835 (Sharjah)	IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
124.	Mount Everest Maritime Incorporation	Registration number 5586846IMO Nr.: 9283019	IRISL front company. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
125.	Narmada Shipping	Aghadir Building, room 306, Dubai, UAE	IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
126.	Newhaven Shipping Company Limited	IMO number of the vessel: 9405930	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
127.	NHL Basic Ltd.	Kattrepelsbrücke 1, 20095 Hamburg, Germany	Owned or controlled by or acting on behalf of IRISL	1.12.2011
128.	NHL Nordland GmbH	Kattrepelsbrücke 1, 20095 Hamburg, Germany	Owned or controlled by or acting on behalf of IRISLIRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
129.	Oxted Shipping Company Limited	Dieudonnee No 1., Triq Tumas Fenech, Qormi, 19635-1114 Malta – Registration number C 38783IMO number of the vessel: 9405942	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
130.	Pacific Shipping	P.O. Box 127137 – Office no 334,Sultan Business Center,Oud Mehta,Dubai, UAE	Acts for IRISL in the Middle East. It is a subsidiary of Azores Shipping Company. Its Managing Director is Mohammad Moghaddami Fard. In October 2010 it was involved in setting up cover companies; the names of the new ones to be used on bills of lading in order to circumvent sanctions. It continues to be involved in the scheduling of IRISL ships.	1.12.2011
131.	Petworth Shipping Company Limited	Dieudonnee No 1., Triq Tumas Fenech, Qormi, 19635-1114 Malta – Registration number C 38781IMO number of the vessel: 9405954	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
132.	Prosper Basic GmbH	Kattrepelsbrücke 1, 20095 Hamburg, Germany	Owned or controlled by or acting on behalf of IRISL	1.12.2011
133.	Prosper Metro Investments Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8320145	Owned or controlled by or acting on behalf of IRISLIRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
134.	Reigate Shipping Companylimited	Dieudonnee No 1., Triq Tumas Fenech, Qormi, 19635-1114 Malta – Registration number C 38782IMO number of the vessel: 9405978	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
135.	Rishi Maritime Incorporation	Registration number 5586850	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
136.	Seibow Logistics Limited (alias Seibow Limited)	111 Futura Plaza, How Ming Street, Kwun Tong, Hong KongRegistration number: 92630	IRISL front company in Hong Kong, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
137.	Shine Star Limited		IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
138.	Silver Universe International Ltd.	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8320157	Owned or controlled by or acting on behalf of IRISL.IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
139.	Sinose Maritime	200 Middle Road 14-03/04, Prime Centre, Singapore 188980	IRISL's head office in Singapore and acts as the exclusive agent of Asia Marine Network. Acts for HDSL in Singapore.	1.12.2011
140.	Sparkle Brilliant Development Limited	Room 1601, Workington Tower, 78 Bonham Strand, Sheung Wan, Hong KongIMO number of the vessel: 8320171	Owned or controlled by or acting on behalf of IRISL.IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
141.	Statira Maritime Incorporation		IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
142.	Tamalaris Consolidated Ltd	P.O. Box 3321, Drake Chambers, Road Town, Tortola, British Virgin Islands	IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
143.	TEU Feeder Limited	143/1 Tower Road, Sliema – Registration number C44939	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
144.	Theta Nari Navigation	143 Tower Road - 1604 Sliema, MaltaRegistration number C 38070	IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
145.	Top Glacier Company Limited		IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
146.	Top Prestige Trading Limited		IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
147.	Tulip Shipping Inc		IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
148.	Western Surge Shipping Company limited (Cyprus)		IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
149.	Wise Ling Shipping Company Limited		IRISL front company, owned or controlled by IRISL or an IRISL affiliate. It is the registered owner of a vessel owned by IRISL or an IRISL affiliate.	1.12.2011
150.	Zeta Neri Navigation	143 Tower Road - 1604 Sliema, MaltaRegistration number C 38069	IRISL front company, owned or controlled by IRISL or an IRISL affiliate.	1.12.2011
151.	BIIS Maritime Limited	Postal address: 147/1 St. Lucia, Valletta, Malta	Owned or controlled by designated Irano Hind	23.1.2012
152.	Darya Delalan Sefid Khazar Shipping Company (Iran) (a.k.a. Khazar Sea Shipping Lines or Darya-ye Khazar Shipping Company or Khazar Shipping Co. or KSSL or Daryaye Khazar (Caspian Sea) Co. or Darya-e-khazar shipping Co.)	Postal address: M. Khomeini St., Ghazian, Bandar Anzil, Gilan, IranNo. 1, End of Shahid Mostafa Khomeini St., Tohid Square, Bandar Anzali, 1711-324, Iran	Owned or controlled by IRISL	23.1.2012
153.	Good Luck Shipping Company LLC(a.k.a. Good Luck Shipping Company)	P.O. Box 5562, Dubai; or P.O. Box 8486, Dubai, United Arab Emirates	Good Luck Shipping Company LLC as the agent for Hafize Darya Shipping Lines (HDS Lines) in the United Arab Emirates provides essential services to HDS Lines which is a designated entity acting on behalf of IRISL.	16.11.2013
154.
155.	Islamic Republic of Iran Shipping Lines (IRISL)	No. 37, Aseman Tower (Sky Tower), Sayyade Shirazee Square, Pasdaran Ave., PO Box 19395-1311, Tehran, Iran;IRISL IMO Nrs: 9051624; 9465849; 7632826; 7632814; 9465760; 8107581; 9226944; 7620550; 9465863; 9226956; 7375363; 9465758; 9270696; 9193214; 8107579; 9193197; 8108559; 8105284; 9465746; 9346524; 9465851; 8112990	IRISL has been involved in the shipment of arms-related materiel from Iran in violation of paragraph 5 of UNSC Resolution 1747(2007). Three clear violations were reported to the UN Security Council Iran Sanctions Committee in 2009.	27.11.2013
156.	Bushehr Shipping Company Limited (a.k.a. Bimeh Iran)	143/1 Tower Road Sliema, Slm 1604, Malta;Registration No. C 37422;c/o Hafiz Darya Shipping Company, No. 60, Ehteshamiyeh Square, 7th Neyestan Street, Pasdaran Avenue, Tehran, Iran;IMO Nr. 9270658	Bushehr Shipping Company Limited is owned by IRISL.	27.11.2013
157.	Hafiz Darya Shipping Lines (HDSL)(a.k.a HDS Lines)	No. 60, Ehteshamiyeh Square, 7th Neyestan Street, Pasdaran Avenue, Tehran, Iran.	HDSL has taken over as beneficial owner a number of Islamic Republic of Iran Shipping Line's (IRISL) vessels. Accordingly, HDSL is acting on behalf of IRISL.	27.11.2013
158.	Irano Misr Shipping Company(a.k.a. Nefertiti Shipping)	6, El Horeya Rd., El Attarein, Alexandria, Egypt;Inside Damietta Port, New Damietta City, Damietta, Egypt;403, El NahdaSt., Port Said, Port Said, Egypt.	Irano Misr Shipping Company as agent for IRISL in Egypt provides essential services to IRISL.	27.11.2013
159.	Irinvestship Ltd	10 Greycoat Place, London SW1P 1SB, United Kingdom;Company Registration Number # 41101 79	Irinvestship Ltd is owned by IRISL.	27.11.2013
160.	IRISL (Malta) Ltd	Flat 1, 143 Tower Road, Sliema SLM 1604, Malta;Registration No. C 33735	IRISL (Malta) Ltd is majority owned by IRISL, through IRISL Europe GmbH, which is in turn owned by IRISL. Accordingly, IRISL Malta Ltd is controlled by IRISL.	27.11.2013
161.	IRISL Europe GmbH (Hamburg)	Schottweg 5, 22087 Hamburg, Germany;V.A.T. Number DE217283818Registration No. HRB 81573	IRISL Europe GmbH (Hamburg) is owned by IRISL.	27.11.2013
162.	IRISL Marine Services and Engineering Company	Sarbandar Gas Station, PO Box 199, Bandar Imam Khomeini, Iran;Karim Khan Zand Avenue (or: Karimkhan Avenue), Iran Shahr Shomai (or: Northern Iranshahr Street), No 221, Tehran, Iran;Shahaid Rajaee Port Road, Kilometer of 8, Before Tavanir Power Station, Bandar Abbas, Iran.	IRISL Marine Services and Engineering Company is controlled by IRISL.	27.11.2013
163.	ISI Maritime Limited (Malta)	147/1 St. Lucia Street, Valetta, Vlt 1185, Malta;Registration No. C 28940c/o IranoHind Shipping Co. Ltd., Mehrshad Street, Sedaghat St., opp. Park Mellat vali-e-asr Ave., Tehran, Iran	ISI Maritime Limited (Malta) is wholly owned by Irano Hind Shipping Company which is in turn majority owned by IRISL. Accordingly, ISI Maritime Limited (Malta) is controlled by IRISL. Irano Hind Shipping Company is designated by the UN as owned, controlled, or acting on behalf of IRISL.	27.11.2013
164.	Khazar Shipping Lines (Bandar Anzali)	End of Shahid Mostafa, Khomeini St., Tohid Square, Bandar Anzali 1711-324, Iran, P.O. Box 43145.	Khazar Shipping Lines is owned by IRISL.	27.11.2013
165.	Marble Shipping Limited(Malta)	143/1 Tower Road, Sliema, Slm 1604, Malta;Registration No. C 41949	Marble Shipping Limited(Malta) is owned by IRISL.	27.11.2013
166.	Safiran Payam Darya (SAPID) Shipping Company(a.k.a. Safiran Payam Darya Shipping Lines, SAPID Shipping Company)	33241 - Narenjestan 8th ST, Artesh Blvd, Aghdasieh, PO Box 19635-1116, Tehran, Iran.	Safiran Payam Darya (SAPID) has taken over as beneficial owner a number of Islamic Republic of Iran Shipping Line's (IRISL) vessels. Accordingly, it is acting on behalf of IRISL.	27.11.2013
167.	Shipping Computer Services Company (SCSCOL)	No 37, Asseman, Shahid Sayyad Shirazees Ave, P.O. Box 1587553-1351, Tehran, Iran.	Shipping Computer Services Company is controlled by IRISL.	27.11.2013
168.	Soroush Saramin Asatir (SSA)(a.k.a. Soroush Sarzamin Asatir Ship Management Company, Rabbaran Omid Darya Ship Management Company, Sealeaders)	No 14 (alt. 5), Shabnam Alley, Fajr Street, Shahid Motahhari Avenue, PO Box 196365-1114, Tehran, Iran.	Soroush Saramin Asatir (SSA) operates and manages a number of Islamic Republic of Iran Shipping Lines (IRISL) vessels. Accordingly, it acts on behalf of IRISL and provides essential services to it.	27.11.2013
169.	South Way Shipping Agency Co. Ltd(a.k.a. Hoopad Darya Shipping Agent)	Hoopad Darya Shipping Agency Company, No 101, Shabnam Alley, Ghaem Magham Street, Tehran, Iran;Bandar Abbas Branch: Hoopad Darya Shipping Agency building, Imam Khomeini Blvd, Bandar Abbas, Iran;Imam Khomieni Branch: Hoopad Darya Shipping Agency building B.I.K. port complex, Bandar Imam Khomeini, Iran;Khorramshahr Branch: Flat no.2-2nd floor, SSL Building, Coastal Blvd, between City Hall and Post Office, Khorramshahr, Iran;Assaluyeh Branch: Opposite to city post office, no.2 telecommunication center, Bandar Assaluyeh, Iran;Chabahar Branch: No address available;Bushehr Branch: No address available.	South Way Shipping Agency Co Ltd manages container terminal operations in Iran and provides fleet personnel services in Bandar Abbas on behalf of IRISL. Accordingly, South Way Shipping Agency Co Ltd is acting on behalf of IRISL.	27.11.2013
170.	Valfajr 8th Shipping Line(a.k.a. Valjafr 8th Shipping Line, Valfajr)	No 119, Corner Shabnam Alley, Shoaa Square, Ghaem Magam Farahani, Tehran, Iran P.O. Box 15875/4155Abyar Alley, Corner of Shahid Azodi St. & Karim Khan Zand Ave., Tehran, Iran;Shahid Azodi St., Karim Khan Zand Ave., Abiar Alley, PO Box 4155, Tehran, Iran.	Valfajr 8th Shipping Line is owned by IRISL.	27.11.2013

ANNEX XWebsites for information on the competent authorities and address for notification to the European CommissionBELGIUMhttps://diplomatie.belgium.be/nl/Beleid/beleidsthemas/vrede_en_veiligheid/sanctieshttps://diplomatie.belgium.be/fr/politique/themes_politiques/paix_et_securite/sanctionshttps://diplomatie.belgium.be/en/policy/policy_areas/peace_and_security/sanctionsBULGARIAhttps://www.mfa.bg/en/101CZECH REPUBLICwww.financnianalytickyurad.cz/mezinarodni-sankce.htmlDENMARKhttp://um.dk/da/Udenrigspolitik/folkeretten/sanktioner/GERMANYhttp://www.bmwi.de/DE/Themen/Aussenwirtschaft/aussenwirtschaftsrecht,did=404888.htmlESTONIAhttp://www.vm.ee/est/kat_622/IRELANDhttp://www.dfa.ie/home/index.aspx?id=28519GREECEhttp://www.mfa.gr/en/foreign-policy/global-issues/international-sanctions.htmlSPAINhttp://www.exteriores.gob.es/Portal/en/PoliticaExteriorCooperacion/GlobalizacionOportunidadesRiesgos/Paginas/SancionesInternacionales.aspxFRANCEhttp://www.diplomatie.gouv.fr/fr/autorites-sanctions/CROATIAhttp://www.mvep.hr/sankcijeITALYhttps://www.esteri.it/mae/it/politica_estera/politica_europea/misure_derogheCYPRUShttp://www.mfa.gov.cy/mfa/mfa2016.nsf/mfa35_en/mfa35_en?OpenDocumentLATVIAhttp://www.mfa.gov.lv/en/security/4539LITHUANIAhttp://www.urm.lt/sanctionsLUXEMBOURGhttps://maee.gouvernement.lu/fr/directions-du-ministere/affaires-europeennes/mesures-restrictives.htmlHUNGARYhttp://www.kormany.hu/download/9/2a/f0000/EU%20szankci%C3%B3s%20t%C3%A1j%C3%A9koztat%C3%B3_20170214_final.pdfMALTAhttps://foreignaffairs.gov.mt/en/Government/SMB/Pages/Sanctions-Monitoring-Board.aspxNETHERLANDShttps://www.rijksoverheid.nl/onderwerpen/internationale-sanctiesAUSTRIAhttp://www.bmeia.gv.at/view.php3?f_id=12750&LNG=en&version=POLANDhttps://www.gov.pl/web/dyplomacjaPORTUGALhttp://www.portugal.gov.pt/pt/ministerios/mne/quero-saber-mais/sobre-o-ministerio/medidas-restritivas/medidas-restritivas.aspxROMANIAhttp://www.mae.ro/node/1548SLOVENIAhttp://www.mzz.gov.si/si/omejevalni_ukrepiSLOVAKIAhttps://www.mzv.sk/europske_zalezitosti/europske_politiky-sankcie_euFINLANDhttp://formin.finland.fi/kvyhteistyo/pakotteetSWEDENhttp://www.ud.se/sanktionerUNITED KINGDOMhttps://www.gov.uk/sanctions-embargoes-and-restrictionsAddress for notifications to the European Commission:European CommissionService for Foreign Policy Instruments (FPI)EEAS 07/99B-1049 Brussels, BelgiumE-mail: relex-sanctions@ec.europa.euANNEX XI

List of products referred to in Article 11(3) and (4)

HS code	Description
270900	Petroleum oils and oils obtained from bituminous minerals, crude

ANNEX XII

LIST OF PRODUCTS REFERRED TO IN ARTICLE 15(3)

HS code	Description
7106	Silver (including silver plated with gold or platinum), unwrought or in semi-manufactured forms, or in powder form
7108	Gold (including gold plated with platinum), unwrought or in semi-manufactured forms, or in powder form
7109	Base metals or silver, clad with gold, not further worked than semi-manufactured
7110	Platinum, unwrought or in semi-manufactured forms, or in powder form
7111	Base metals, silver or gold, clad with platinum, not further worked than semi-manufactured
7112	Waste and scrap of precious metal or of metal clad with precious metal; other waste and scrap containing precious metal or precious-metal compounds, of a kind used principally for the recovery of precious metal

ANNEX XIIIList of persons, entities and bodies referred to in Article 23a(1)A.Natural personsB.Entities and bodiesANNEX XIVList of persons, entities and bodies referred to in Article 23a(2)A.Natural personsB.Entities and bodies