Commission Implementing Regulation (EU) 2019/1083 of 21 June 2019 amending Council Regulation (EU) 2017/1509 concerning restrictive measures against the Democratic People's Republic of Korea

In forceVersion 2019-06-21from 2019-07-01

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Contents

Preamble
1. Article 1
2. Article 2
ANNEX
ANNEX
ANNEX II Goods and technology referred to in points (a) and (c) of Article 3(1) and in Article 7
PART I
PART II
II.A0. a.
II.A1. Technical note: Technical note: Technical notes: 1.2.
II.A1. a.
II.A1. Technical note: Technical note: a.
II.A2. Technical note:
II.A2. a.
II.A3. Technical notes: 1.2.
II.A3. a.
II.A6. Notes: 1.2.
II.A6. a.
II.A7. a.
1. a.
3. a.
PART III
PART IV
IV.A0. Ring Magnets
i.
ii.
iii.
IV.A1. i.
i.
ii.
IV.A2.
PART V
PART VI
VI.A1.
PART VII
VII.A1. Note: Note: Notes: 1.2. Notes: 1.2.3.4.
VII.A1. Note:
5. a.
2. a.
3. a.
(d)
6. a.
6. a.
7. a.
VII.A1. Note: Note:
2. a.
4. a.
1. a.
VII.A1. Note: Note: Notes: 1.2.
1. a.
2. a.
VII.A1. Note: Note: Notes: 1.2. Notes: 1.2.
VII.A1. Note: Note: Notes: 1.2. Notes: 1.2.3.
VII.A4.
1. a.
VII.A5.
VII.A6 Technical note: Notes: 1.2. Note:
VII.A6
VII.A6 Technical note:
VII.A6 Technical note: Notes: 1.2.
2. a.
1. a.
4. a.
VII.A7. Notes: 1.2.
VII.A7.
1. a.
2. a.
VII.A8.
4. a.
VII.A9.
(a)
(b)
1. a.
2. a.
PART VIII
VIII.A3.
PART IX
IX.A1.
IX.A2. (a) Technical notes: 1.2.
1. a.
2. a.
1. a.
IX.A3.4. Notes: 1.2. Notes: 1.2. Technical notes: 1.2. Technical note: Technical notes: 1.2.3.4.5.6.7. Technical notes: 1.2.3.4. Notes: 1.2. Technical notes: 1.2.
IX.A3. (a) Notes: 1.2.
IX.A3.4.
4. a.
5. a.
IX.A3.4. Notes: 1.2. a.
IX.A3.4. Notes: 1.2. Notes: 1.2.
IX.A3.4. Notes: 1.2. Notes: 1.2. Technical notes: 1.2. Technical note:
IX.A3.4. Notes: 1.2. Notes: 1.2. Technical notes: 1.2. Technical note: Technical notes: 1.2.3.4.5.6.7.
IX.A3.4. Notes: 1.2. Notes: 1.2. Technical notes: 1.2. Technical note: Technical notes: 1.2.3.4.5.6.7. Technical notes: 1.2.3.4.
2. a.
IX.A3.4. Notes: 1.2. Notes: 1.2. Technical notes: 1.2. Technical note: Technical notes: 1.2.3.4.5.6.7. Technical notes: 1.2.3.4. Notes: 1.2.
1. Technical notes: 1.2.
1. a.
4. a.
1. a.
3. a.
IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2. Technical note: Notes: 1.2. Technical note: 1. Technical note: Technical notes: 1.2.
IX.A6.
3. a.
5. a.
6. a.
1. a.
IX.A6. Technical notes: 1.2. a.
2. a.
3. a.
1. a.
4. a.
IX.A6. Technical notes: 1.2. Notes: 1.2.
IX.A6. Technical notes: 1.2. Notes: 1.2.3.
3. Technical note:
4. a.
1. a.
2. a.
3. a.
5. a.
6. a.
IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2.
IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2. Technical note:
1. a.
2. a.
3. a.
IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2. Technical note: Notes: 1.2. a.
1. a.
2. a.
3. a.
IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2. Technical note: Notes: 1.2. Technical note: a.
3. a.
1. Technical note:
3. a.
IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2. Technical note: Notes: 1.2. Technical note: 1.
(b)
2. Technical notes: 1.2.
IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2. Technical note: Notes: 1.2. Technical note: 1. Technical note:
1. a.
2. a.
IX.A7. Technical note: Technical note:
IX.A7.
IX.A7. Technical note:
IX.A8. Technical note:
IX.A8.
4. a.
IX.A9.
(b)
1. a.
(a)
2. a.
3. a.

THE EUROPEAN COMMISSION,

Having regard to the Treaty on the Functioning of the European Union,

Having regard to Council Regulation (EU) 2017/1509 of 30 August 2017 concerning restrictive measures against the Democratic People's Republic of Korea, and in particular Article 46(b) thereof,

Whereas:

(1) Council Regulation (EU) 2017/1509 gives effect to measures provided for in Council Decision (CFSP) 2016/849.

(2) On 5 August and 11 September 2017, the United Nations Security Council adopted Resolutions (UNSCR) 2371 (2017) and 2375 (2017) respectively providing for new measures against North Korea. In accordance with paragraphs 4 and 5 of Resolution UNSCR 2371 (2017) and paragraphs 4 and 5 of Resolution UNSCR 2375 (2017), on 22 August, 5 September, 29 September and 2 October 2017, the Sanctions Committee established pursuant to Resolution UNSCR 1718 (2006) published four lists of additional conventional arms and weapons of mass destruction-related items, materials, equipment, goods, and technology to which prohibitions on the supply, procurement, transfer, as well as the prohibitions related to technical and financial assistance apply.

(3) Following the adoption of Resolutions UNSCR 2371 (2017) and 2375 (2017), on 14 September and 10 October 2017 respectively the Council adopted Decision (CFSP) 2017/1562 and Decision (CFSP) 2017/1838. Council Regulation (EU) 2017/1548 and Council Regulation (EU) 2017/1836 amended Council Regulation (EU) No 2017/1509 accordingly, by adding parts VI, VII, VIII and IX to Annex II as well as a reference to the relevant UN lists.

(4) The goods and technology to be included in parts VI, VII, VIII and IX of Annex II of Regulation (EU) 2017/1509 and the related categories in Council Regulation No 428/2009 should be identified. Parts I, II, III, IV and V of Annex II should be amended to reflect the structure used in parts VI, VII, VIII and IX.

(5) Annex II of Council Regulation (EU) 2017/1509 should therefore be amended accordingly,

HAS ADOPTED THIS REGULATION:

Article 1

Annex II to Regulation (EU) 2017/1509 is amended in accordance with the Annex to this Regulation.

Article 2

This Regulation shall enter into force on the fifth day following that 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. Done at Brussels, 21 June 2019. For the Commission, On behalf of the President, Head of the Service for Foreign Policy Instruments

ANNEX

Annex II to Council Regulation (EU) 2017/1509 is replaced by the following:

ANNEX II Goods and technology referred to in points (a) and (c) of Article 3(1) and in Article 7

The notes, acronyms and abbreviations, and the definitions in Annex I to Regulation (EC) No 428/2009 apply for the purpose of this Annex.

PART I

All goods and technology listed in Annex I to Regulation (EC) No 428/2009.

PART II

Other items, materials, equipment, goods and technology which could contribute to DPRK's nuclear-related, other weapons of mass destruction-related or ballistic missile-related programmes. Unless otherwise stated, reference numbers used in the column entitled Description refer to the descriptions of dual use items and technology set out in Annex I to Regulation (EC) No 428/2009. 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. Definitions of terms between single quotation marks are given in a technical note to the relevant item. Definitions of terms between "double quotation marks" can be found in Annex I to Regulation (EC) No 428/2009, except the following:

GENERAL NOTES

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. Goods specified in this Annex include both new and used goods.

GENERAL TECHNOLOGY NOTE (GTN) (To be read in conjunction with Part C)

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 prohibited in Part A (Goods), is prohibited in accordance with the provisions of Part B. The "technology" "required" for the "development", "production" or "use" of prohibited goods remains under prohibition even when applicable to non-prohibited goods. 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. 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.

GOODS

II.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: N/A II.A0.002 Faraday isolators in the wavelength range 500 nm – 650 nm. N/A II.A0.003 Optical gratings in the wavelength range 500 nm – 650 nm. N/A 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. N/A II.A0.005 Nuclear reactor vessel components and testing equipment, other than those specified in 0A001, as follows: 0A001 II.A0.006 Nuclear detection systems, other than those specified in 0A001.j. or 1A004.c., for detection, identification or quantification of radioactive materials or radiation of nuclear origin and specially designed components thereof. N.B: For personal equipment refer to II.A1.004 below. 0A001.j. 1A004.c. II.A0.007 Bellows-sealed valves other than those specified in 0B001.c.6., 2A226 or 2B350, made of aluminium alloy or stainless steel type 304, 304L or 316L. 0B001.c.6. 2A226 2B350 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: 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. N/A

II.A0. a.

Iodine hollow cathode lamps with windows in pure silicon or quartz;

Uranium hollow cathode lamps.

Seals;

Internal components;

Sealing, testing and measurement equipment.

Turbo-molecular pumps having a flow-rate equal to or greater than 400 l/s;

Roots type vacuum roughing pumps having a volumetric aspiration flow-rate greater than 200 m3/h;

Bellows-sealed, scroll, dry compressor, and bellows-sealed, scroll, dry vacuum pumps.

II.A1. Technical note: Technical note: Technical notes: 1.2.

SPECIAL MATERIALS AND RELATED EQUIPMENT No Description Related item from Annex I to Regulation (EC) No 428/2009 II.A1.001 Bis(2-ethylhexyl) phosphoric acid (HDEHP or D2HPA) Chemical Abstract Number (CAS): [CAS 298-07-7] solvent in any quantity, with a purity greater than 90 %. N/A II.A1.002 Fluorine gas CAS: [7782-41-4], with a purity of at least 95 %. N/A II.A1.003 Ring-shaped seals and gaskets, having an inner diameter of 400 mm or less, made of any of the following materials: 1A001 II.A1.004 Personal equipment for detecting radiation of nuclear origin, other than that specified in 1A004.c., including personal dosimeters. 1A004.c. II.A1.005 Electrolytic cells for fluorine production, other than those specified in 1B225, with an output capacity greater than 100 g of fluorine per hour. 1B225 II.A1.006 Catalysts, other than those specified in 1A225 or 1B231, 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. 1A225 1B231 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: The phrase alloys capable of encompasses alloys before or after heat treatment. 1C002.b.4. 1C202.a. II.A1.008 Magnetic metals, of all types and of whatever form, other than those specified in 1C003.a. having an initial relative permeability of 120000 or more and a thickness between 0,05 mm and 0,1 mm. Measurement of initial relative permeability must be performed on fully annealed materials. 1C003.a. II.A1.009 Fibrous or filamentary materials or prepregs, other than those specified in 1C010.a., 1C010.b., 1C210.a. or 1C210.b., as follows: 1C010.a. 1C010.b. 1C210.a. 1C210.b. II.A1.010 Resin-impregnated or pitch-impregnated fibres (prepregs), metal or carbon-coated fibres (preforms) or carbon fibre preforms, as follows: 1C010 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 Not used. II.A1.013 Tantalum, tantalum carbide, tungsten, tungsten carbide and alloys thereof, other than those specified in 1C226, having both of the following characteristics: 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. Technical note: Elemental powder means a high purity powder of one element. N/A 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. N/A II.A1.016 Maraging steel, other than those specified by 1C116 or 1C216. The phrase maraging steel capable of encompasses maraging steel before or after heat treatment. 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. 1C116 1C216 II.A1.017 Metals, metal powders and material as follows: 1C117 1C226 II.A1.018 Soft magnetic alloys, other than those specified in 1C003, having a chemical composition as follows: 1C003 II.A1.019 Not used. II.A1.020 Graphite, other than that specified in 0C004 or 1C107.a., designed or specified for use in Electrical Discharge Machining (EDM) machines. 0C004 1C107.a. II.A1.021 Steel alloys in sheet or plate form, having any of the following characteristics: Note: the phrase alloys capable of encompasses alloys before or after heat treatment. Technical 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. 1C116 1C216 II.A1.022 Carbon-Carbon Composite material. 1A002.b.1 II.A1.023 Nickel alloys in crude or semi-fabricated form, containing 60 % by weight or more nickel. 1C002.c.1.a II.A1.024 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.A1.025 Titanium alloys, other than those specified in 1C002 and 1C202. 1C002 1C202 II.A1.026 Zirconium and zirconium alloys, other than those specified in 1C011, 1C111 and 1C234. 1C011 1C111 1C234 II.A1.027 Explosive materials other than those specified in 1C239, or materials or mixtures containing more than 2 % by weight of such explosive materials, with a crystalline density higher than 1,5 g/cm3 and with a detonation speed higher than 5000 m/s. 1C239

II.A1. a.

Copolymers of vinylidene fluoride having 75 % or more beta crystalline structure without stretching;

Fluorinated polyimides containing 10 % by weight or more of combined fluorine;

Fluorinated phosphazene elastomers containing 30 % by weight or more of combined fluorine;

Polychlorotrifluoroethylene (PCTFE, e.g. Kel-F ®);

Fluoro-elastomers (e.g. Viton ®, Tecnoflon ®);

Polytetrafluoroethylene (PTFE).

Capable of an ultimate tensile strength of 460 MPa or more at 293 K (20 °C); or

Having a tensile strength of 415 MPa or more at 298 K (25 °C).

II.A1. Technical note: Technical note: a.

Aramid fibrous or filamentary materials having either of the following characteristics:

1. A specific modulus exceeding 10 × 106 m; or

2. A specific tensile strength exceeding 17 × 104 m;

Glass Gfibrous or filamentary materials having either of the following characteristics:

1. A specific modulus exceeding 3,18 × 106 m; or

2. A specific tensile strength exceeding 76,2 × 103 m;

Thermoset resin-impregnated continuous yarns, rovings, tows or tapes with a width of 15 mm or less (once prepregs), made from glass fibrous or filamentary materials other than those specified in I.A1.010.a. below;

Carbon fibrous or filamentary materials;

Thermoset resin-impregnated continuous yarns, rovings, tows, or tapes, made from carbon fibrous or filamentary materials;

Polyacrylonitrile (PAN) continuous yarns, rovings, tows or tapes;

Para-aramid fibrous or filamentary materials (Kevlar® and other Kevlar®-like fibres).

Made from fibrous or filamentary materials specified in II.A1.009 above;

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;

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.

In forms having a hollow cylindrical or spherical symmetry (including cylinder segments) with an inside diameter between 50 mm and 300 mm; and

A mass greater than 5 kg.

II.A1. Technical note: Technical note: Technical notes: 1.2. a.

Tungsten and tungsten alloys, other than those specified in 1C117, in the form of uniform spherical or atomized particles of 500 μm (micrometre) diameter or less with a tungsten content of 97 % by weight or more;

Molybdenum and molybdenum alloys, other than those specified in 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;

Tungsten materials in the solid form, other than those specified in 1C226 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; or

3. Silver infiltrated tungsten containing 80 % by weight or more of tungsten.

Iron content between 30 % and 60 %; and

Cobalt content between 40 % and 60 %.

(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.

II.A2. Technical note:

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: 2B116 II.A2.002 Machine tools, other than those specified in 2B001 or 2B201 and any combination thereof, for removing (or cutting) metals, ceramics, or composites that, according to the manufacturer's technical specification, can be equipped with electronic devices for numerical control, having positioning accuracies of equal to or less (better) than 30 μm according to ISO 230/2 (1988) or national equivalents along any linear axis. Technical note: Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of the Member State in which they are established. 2B001 2B201 II.A2.002a Components and numerical controls, specially designed for machine tools specified in 2B001, 2B201 or I.A2.002 above. N/A II.A2.003 Balancing machines and related equipment as follows: 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: 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. 2B225 II.A2.005 Controlled atmosphere heat treatment furnaces or oxidation furnaces capable of operation at temperatures above 400 °C. Note: 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. 2B226 2B227 II.A2.006 Not used. 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: Technical note: For the purposes of 2B230 accuracy includes non-linearity, hysteresis and repeatability at ambient temperature. 2B230 II.A2.008 Liquid-liquid contacting equipment (mixer-settlers, pulsed columns, plate 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 any of the following materials: 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.A2.009 Industrial equipment and components, other than those specified in 2B350.d., as follows: 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 made from any of the following materials: 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.A2.010 Multiple-seal, and seal-less pumps, other than those specified in 2B350.i, suitable for corrosive fluids, or vacuum pumps 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 any of the following materials: Technical notes: The materials used for gaskets and seals and other implementations of sealing functions do not determine the status of control of the pump. The term rubber encompasses all kinds of natural and synthetic rubbers. 2B350.i. II.A2.011 Centrifugal separators, other than those specified in 2B352.c., capable of continuous separation without the propagation of aerosols and manufactured from: Centrifugal separators include decanters. 2B352.c. II.A2.012 Sintered metal filters, other than those specified in 2B352.d., made of nickel or nickel alloy with more than 40 % nickel by weight. 2B352.d. II.A2.013 Spin-forming machines and flow-forming machines, other than those specified by 2B009, 2B109 or 2B209 and specially designed components therefor. Technical note: For the purpose of this item, machines combining the functions of spin-forming and flow-forming are regarded as flow-forming machines. 2B009 2B109 2B209 II.A2.014 Equipment and reagents, other than those specified in 2B350 or 2B352, as follows: 2B350 2B352 II.A2.015 Equipment, other than that specified in 2B005, 2B105 or 3B001.d., for the deposition of metallic overlays as follows, and specially designed components and accessories therefor: 2B005 2B105 3B001.d. II.A2.016 Open tanks or containers, with or without agitators, with a total internal (geometric) volume greater than 0,5 m3 (500 litres), where all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials: Technical note: The term rubber encompasses all kinds of natural and synthetic rubbers. 2B350

II.A2. 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;

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 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.

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.;

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.

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 unbalance in two planes or more; and

4. Capable of balancing to a residual specific unbalance of 0,2 g × mm per kg of rotor mass;

Indicator heads designed or modified for use with machines specified in a. above.

A capability of penetrating a hot cell wall of 0,3 m or more (through the wall operation); or

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).

Pressure sensing elements made of or protected by Materials resistant to corrosion by uranium hexafluoride (UF6); and

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; or

2. A full scale of 200 kPa or greater and an accuracy of better than 2 kPa.

Alloys with more than 25 % nickel and 20 % chromium by weight;

Fluoropolymers;

Glass (including vitrified or enamelled coating or glass lining);

Graphite or carbon graphite;

Nickel or alloys with more than 40 % nickel by weight;

Tantalum or tantalum alloys;

Titanium or titanium alloys;

Zirconium or zirconium alloys; or

Stainless steel.

Alloys with more than 25 % nickel and 20 % chromium by weight;

Fluoropolymers;

Glass (including vitrified or enamelled coating or glass lining);

Graphite or carbon graphite;

Nickel or alloys with more than 40 % nickel by weight;

Tantalum or tantalum alloys;

Titanium or titanium alloys;

Zirconium or zirconium alloys;

Silicon carbide;

Titanium carbide; or

Stainless steel.

Alloys with more than 25 % nickel and 20 % chromium by weight;

Ceramics;

Ferrosilicon;

Fluoropolymers;

Glass (including vitrified or enamelled coatings or glass lining);

Graphite or carbon graphite;

Nickel or alloys with more than 40 % nickel by weight;

Tantalum or tantalum alloys;

Titanium or titanium alloys;

Zirconium or zirconium alloys;

Niobium (columbium) or niobium alloys;

Stainless steel;

Aluminium alloys; or

Rubber.

Alloys with more than 25 % nickel and 20 % chromium by weight;

Fluoropolymers;

Glass (including vitrified or enamelled coating or glass lining);

Nickel or alloys with more than 40 % nickel by weight;

Tantalum or tantalum alloys;

Titanium or titanium alloys; or

Zirconium or zirconium alloys.

II.A2. Technical note: a.

Fermenters capable of cultivation of pathogenic micro-organisms or viruses, or capable of toxin production, without the propagation of aerosols, and having a total capacity of 10 l or more;

Agitators for fermenters as mentioned in a. above; Technical Note: Fermenters include bioreactors, chemostats and continuous-flow systems.

Laboratory equipment as follows:

1. Polymerase chain reaction (PCR)-equipment

2. Genetic sequencing equipment;

3. Genetic synthesizers;

4. Electroporation equipment;

5. Specific reagents associated with the equipment in I.A2.014.c. numbers 1. to 4. above;

Filters, micro-filters, nano-filters or ultra-filters usable in industrial or laboratory biology for continuous filtering, except filters specially designed or modified for medical or clear water production purposes and to be used in the framework of EU or UN officially supported projects;

Ultracentrifuges, rotors and adaptors for ultracentrifuges;

Freeze drying equipment.

Chemical vapour deposition (CVD) production equipment;

Physical vapour deposition (PVD) production equipment;

Production equipment for deposition by means of inductive or resistance heating.

Alloys with more than 25 % nickel and 20 % chromium by weight;

Fluoropolymers;

Glass (including vitrified or enamelled coatings or glass lining);

Nickel or alloys with more than 40 % nickel by weight;

Tantalum or tantalum alloys;

Titanium or titanium alloys;

Zirconium or zirconium alloys;

Niobium (columbium) or niobium alloys;

Stainless steel;

Wood; or

Rubber.

II.A3. Technical notes: 1.2.

ELECTRONICS No Description Related item from Annex I to Regulation (EC) No 428/2009 II.A3.001 High voltage direct current power supplies, other than those specified in 0B001.j.5. or 3A227, having both of the following characteristics: 0B001.j.5. 3A227 II.A3.002 Mass spectrometers, other than those specified in 0B002.g. or 3A233, 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 therefor: 0B002.g. 3A233 II.A3.003 Frequency changers or generators, other than those specified by 0B001.b.13. or 3A225, having all of the following characteristics, and specially designed components and software therefor: Frequency changers are also known as converters, inverters, generators, electronic test equipment, AC power supplies, variable speed motor drives or variable frequency drives. The functionality specified in this item may be met by certain equipment marketed as: electronic test equipment, AC power supplies, variable speed motor drives or variable frequency drives. 0B001.b.13. 3A225 II.A3.004 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. N/A

II.A3. 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; and

Current or voltage stability better than 0,1 % over a time period of four hours.

Inductively coupled plasma mass spectrometers (ICP/MS);

Glow discharge mass spectrometers (GDMS);

Thermal ionisation mass spectrometers (TIMS);

Electron bombardment mass spectrometers which have a source chamber constructed from, lined with or plated with materials resistant to corrosion by uranium hexafluoride UF6;

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; or

2. A source chamber constructed from, lined with or plated with materials resistant to UF6;

Mass spectrometers equipped with a micro-fluorination ion source designed for actinides or actinide fluorides.

Multiphase output capable of providing a power of 40 W or greater;

Capable of operating in the frequency range between 600 and 2000 Hz; and

Frequency control better (less) than 0,1 %.

II.A6. Notes: 1.2.

SENSORS AND LASERS No Description Related item from Annex I to Regulation (EC) No 428/2009 II.A6.001 Yttrium aluminium garnet (YAG) rods. N/A II.A6.002 Optical equipment and components, other than those specified in 6A002 or 6A004.b. as follows: Infrared optics in the wavelength range 9 μm – 17 μm and components thereof, including cadmium telluride (CdTe) components. 6A002 6A004.b. II.A6.003 Wave front corrector systems, other than mirrors specified in 6A004.a., 6A005.e. or 6A005.f., 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. 6A004.a. 6A005.e. 6A005.f. II.A6.004 Argon ion lasers, other than those specified in 0B001.g.5., 6A005.a.6. and/or 6A205.a., having an average output power equal to or greater than 5 W. 0B001.g.5. 6A005.a.6. 6A205.a. II.A6.005 Semiconductor lasers, other than those specified in 0B001.g.5., 0B001.h.6. or 6A005.b., and components thereof, as follows: Semiconductor lasers are commonly called laser diodes. This item does not cover laser diodes with a wavelength in the range 1,2 μm – 2,0 μm. 0B001.g.5. 0B001.h.6. 6A005.b. II.A6.006 Tunable semiconductor lasers and tunable semiconductor laser arrays, other than those specified in 0B001.h.6. or 6A005.b., 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. Note: Semiconductor lasers are commonly called laser diodes. 0B001.h.6. 6A005.b. II.A6.007 Solid state tunable lasers, other than those specified in 0B001.g.5., 0B001.h.6. or 6A005.c.1., and specially designed components thereof, as follows: 0B001.g.5. 0B001.h.6. 6A005.c.1. II.A6.008 Neodymium-doped (other than glass) lasers, other than those specified in 6A005.c.2.b., having an output wavelength greater than 1,0 μm but not exceeding 1,1 μm and output energy exceeding 10 J per pulse. 6A005.c.2.b. II.A6.009 Components of acousto-optics, as follows: 6A203.b.4. 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, other than those specified in 0B001.g.5., 6A005 and or 6A205.c., having all of the following characteristics: Note: This item does not cover single mode oscillators. 0B001.g.5. 6A005 6A205.c. II.A6.012 Pulsed carbon dioxide lasers, other than those specified in, 0B001.h.6., 6A005.d. or 6A205.d., having all of the following characteristics: 0B001.h.6. 6A005.d. 6A205.d. II.A6.013 Lasers, other than those specified in 6A005 or 6A205. 6A005 6A205

II.A6. a.

Individual semiconductor lasers with an output power greater than 200 mW each, in quantities larger than 100;

Semiconductor laser arrays having an output power greater than 20 W.

II.A6. Notes: 1.2. a.

Titanium-sapphire lasers,

Alexandrite lasers.

Framing tubes and solid-state imaging devices having a recurrence frequency equal to or exceeding 1 kHz;

Recurrence frequency supplies;

Pockels cells.

Operating at wavelengths between 300 nm and 800 nm;

An average output power greater than 10 W but not exceeding 30 W;

A repetition rate greater than 1 kHz; and

Pulse width less than 100 ns.

Operating at wavelengths between 9 μm and 11 μm;

A repetition rate greater than 250 Hz;

An average output power greater than 100 W but not exceeding 500 W; and

Pulse width less than 200 ns.

II.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: 7A001 7A003 7A101 7A103

II.A7. a.

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:

1. 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. a.

Navigation error (free inertial) subsequent to normal alignment of 0,8 nautical mile per hour (nm/hr) Circular Error Probable (CEP) or less (better); or

Specified to function at linear acceleration levels exceeding 10 g;

2. 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);

3. Inertial Equipment for Azimuth, Heading, or North Pointing having any of the following characteristics, and specially designed components thereof:

3. a.

Designed to have an Azimuth, Heading, or North Pointing accuracy equal to, or less (better) than 6 arc minutes RMS at 45 degrees latitude; or

Designed to have a non-operating shock level of at least 900 g at a duration of at least 1 msec.

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.

c. Technical notes: 1.2.

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 down-hole well services operations. Note: The parameters of a.1. and a.2. are applicable with any of the following environmental conditions: a.2. 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. 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.

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:

1. a.

A constant power spectral density (PSD) value of 0,04 g2/Hz over a frequency interval of 15 to 1000 Hz; and

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); or

3. According to national standards equivalent to 1. or 2. above.

II.A9. AEROSPACE AND PROPULSION No Description Related item from Annex I to Regulation (EC) No 428/2009 II.A9.001 Explosive bolts. N/A II.A9.002 Internal combustion engines (i.e. axial piston or rotary piston type), designed or modified for propelling aircrafts or lighter-than-air-vehicles and specially designed components therefor. N/A II.A9.003 Trucks, other than those specified in 9A115, having more than one motorised axle and a payload exceeding 5 tonnes. Note: This item includes flatbed trailers, semi trailers and other trailers. 9A115

SOFTWARE No Description Related item from Annex I to Regulation (EC) No 428/2009 II.B.001 Software required for the development, production or use of the items in Part A. (Goods). N/A

TECHNOLOGY No Description Items, materials, equipment, goods and technology Related item from Annex I to Regulation (EC) No 428/2009 II.C.001 Technology required for the development, production or use of the items in Part A. (Goods). N/A

PART III

Other items, materials, equipment, goods and technology which could contribute to DPRK's ballistic-missile sector.

GOODS

III.A1. SPECIAL MATERIALS AND RELATED EQUIPMENT No Description Related item from Annex I to Regulation (EC) No 428/2009 III.A1.001 Unwrought aluminium 1C002 III.A1.002 Aluminium waste and scrap 1C002 III.A1.003 Aluminium powders and flakes 1C111 III.A1.004 Aluminium bars, rods and profiles 1C002 III.A1.005 Aluminium wire 1C002 III.A1.006 Aluminium plates, sheets and strip, of a thickness exceeding 0,2 mm 1C002 III.A1.007 Aluminium tubes and pipes 1C002 III.A1.008 Aluminium tube or pipe fittings (for example, couplings, elbows, sleeves) 1C002 III.A1.009 Stranded wire, cables, plaited bands and the like, of aluminium, not electrically insulated 1C002

PART IV

Weapons of mass destruction-related items, materials, equipment, goods and technology identified and designated pursuant to paragraph 25 of UN Security Council Resolution 2270 (2016).

GOODS

IV.A0. NUCLEAR MATERIALS, FACILITIES AND EQUIPMENT No Description Related item from Annex I to Regulation (EC) No 428/2009 IV.A0.001 3A201.b. IV.A0.002 0B001.b.13. 3A225

IV.A0. Ring Magnets

Permanent magnet materials having both the following characteristics:

i.

Ring-shaped magnet with a relation between outer and inner diameter smaller or equal to 1.6:1; and

ii.

Made of any of the following magnetic materials: aluminium-nickel-cobalt, ferrites, samarium-cobalt, or neodymium-iron-boron.

Frequency Changers (also known as converters or inverters) Technical Notes: (1)(2)

Frequency changers, other than those specified in entries 0B001.b.13 or 3A225 of Annex 1, having all of the following characteristics, and specially designed software therefore: Frequency changers are also known as converters or inverters. The functionality specified above may be met by certain equipment described or marketed as electronic test equipment, AC power supplies, variable speed motor drives, or variable frequency drives.

Frequency Changers (also known as converters or inverters)

i.

Multiphase frequency output;

ii.

Capable of providing a power of 40 W or greater; and

iii.

Capable of operating anywhere (at any one point or more) within the frequency range of between 600 and 2000 Hz.

IV.A1. SPECIAL MATERIALS AND RELATED EQUIPMENT No Description Related item from Annex I to Regulation (EC) No 428/2009 IV.A1.001 Maraging steel having both the following characteristics: 1C216 IV.A1.002 Magnetic alloy materials in sheet or thin strip form having both of the following characteristics: 1C005 IV.A1.003 1C202 IV.A1.004 Fibrous or filamentary materials and prepregs, as follows: 1C210 IV.A1.005 Filament winding machines and related equipment, as follows: 1B201 IV.A1.006 Metal hydrides such as, zirconium 1B231 IV.A1.007 Sodium metal (7440-23-5) 1C350 IV.A1.008 Sulphur trioxide (7446-11-9) 1C350 IV.A1.009 Aluminium chloride (7446-70-0) N/A IV.A1.010 Potassium Bromide (7758-02-3) 1C350 IV.A1.011 Sodium bromide (7647-15-6) 1C350 IV.A1.012 Dichloromethane (75-09-2) 1C350 IV.A1.013 Isopropyl bromide (75-26-3) 1C350 IV.A1.014 Isopropyl ether (108-20-3) 1C350 IV.A1.015 Monoisopropylamine (75-31-0) 1C350 IV.A1.016 Trimethylamine (75-50-3) 1C350 IV.A1.017 Tributylamine (102-82-9) 1C350 IV.A1.018 Triethylamine (121-44-8) 1C350 IV.A1.019 N,N-Dimethylaniline (121-69-7) 1C350 IV.A1.020 Pyridine (110-86-1) 1C350

IV.A1. i.

capable of an ultimate tensile strength of 1500 MPa or more at 293 K (20 °C).

ii.

In bar or tube form, with an outer diameter of 75 mm or greater.

(a) Thickness of 0,05 mm or less; or height of 25 mm or less, and

(b) Made of any of the following magnetic alloy materials: iron-chromium-cobalt, iron-cobalt-vanadium, iron- chromium-cobalt-vanadium, or iron-chromium.

High-strength Aluminium Alloy Technical Note:

Aluminium alloys having both the following characteristics: The phrase capable of encompasses aluminium alloy before or after heat treatment.

High-strength Aluminium Alloy

i.

capable of an ultimate tensile of strength of 415 MPa or more at 293 K (20 °C) and

ii.

In bar or tube form, with an outer diameter of 75 mm or greater.

Carbon, aramid, or glass fibrous or filamentary materials having both of the following characteristics:

(1) A specific modulus exceeding 3,18 × 106 m; and

(2) A specific tensile strength exceeding 76,2 × 103 m;

ii.

Prepregs: Thermoset resin-impregnated continuous yarns, rovings, tows or tapes with a width of 30 mm or less, made from carbon, aramid, or glass fibrous or filamentary materials controlled in (a) above.

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; and

(3) Capable of winding cylindrical tubes of diameter of 75 mm or greater;

ii.

Coordinating and programming controls for filament winding machines specified in (a) above;

iii.

Mandrels for filament winding machines specified in (a) above.

IV.A2. MATERIALS PROCESSING No Description Related item from Annex I to Regulation (EC) No 428/2009 IV.A2.001 Flow-forming Machines As described in INFCIRC/254/Rev.9/Part2 and S/2014/253 2B209 IV.A2.002 Laser welding equipment N/A IV.A2.003 4- and 5-axis CNC machine tools 2B201 IV.A2.004 Plasma cutting equipment N/A IV.A2.005 Reaction vessels, reactors, agitators, heat exchangers, condensers, pumps, valves, storage tanks, containers, receivers, and distillation or absorption columns that meet performance parameters described in S/2006/853 and S/2006/853/corr.1 Single-seal pumps with manufacturer's specified maximum flow-rate greater than 0,6 m3/h and casings (pump bodies), preformed casing liners, impellers, rotors or jet pump nozzles designed for such pumps, in which all surfaces that come into direct contact with the chemical(s) being processed are made from any of the following materials: 2B350 IV.A2.006 Conventional or turbulent air-flow clean-air rooms and self-contained fan-HEPA filter units that could be used for P3 or P4 (BSL 3, BSL 4, L3, L4) containment facilities. 2B352

IV.A2.

(a) nickel or alloys with more than 40 % nickel by weight;

(b) alloys with more than 25 % nickel and 20 % chromium by weight;

(d) glass or glass-lined (including vitrified or enamelled coating);

(e) graphite or carbon-graphite;

(f) tantalum or tantalum alloys;

(g) titanium or titanium alloys;

(h) zirconium or zirconium alloys;

(i) ceramics;

(j) ferrosilicon (high silicon iron alloys); or

(k) niobium (columbium) or niobium alloys.

PART V

Weapons of mass destruction-related items, materials, equipment, goods and technology identified and designated pursuant to paragraph 4 of UN Security Council Resolution 2321 (2016).

GOODS

V.A1. SPECIAL MATERIALS AND RELATED EQUIPMENT No Description Related item from Annex I to Regulation (EC) No 428/2009 V.A1.001 Isocyanates (TDI (Toluene di-isocyanate), MDI (Methylene bis (phenyl isocyanate)), IPDI (Isophorone diiosocyanate), HNMDI or HDI (Hexamethylene diisocyanate), and DDI (dimeryl diisocyanate) and production equipment. N/A V.A1.002 Ammonium nitrate, chemically pure or in phase stabilized version (PSAN). 1C111 V.A1.003 Polymeric Substances (Hydroxyl Terminated Poly-Ether (HTPE), Hydroxyl Terminated Caprolactone Ether (HTCE), Polypropylene glycol (PPG), Polydiethyleneglycol adipate (PGA) and Polyethylene 1C111 V.A1.004 Manganese metal Brazing Foils. 1C111

V.A2. MATERIALS PROCESSING No Description Related item from Annex I to Regulation (EC) No 428/2009 V.A2.001 Hydroforming machines. 2B109 V.A2.002 Thermal treatment furnaces — Temperature > 850 °C and one dimension > 1 m, II.A2.005 2B226 2B227 V.A2.003 Electrical Discharge Machines (EDMs) 2B001.d V.A2.004 Friction stir welding machines. N/A V.A2.005 Floor-mounted fume hoods (walk-in style) with a minimum nominal width of 2,5 meters, 2B352 V.A2.006 Batch centrifuges with a rotor capacity of 4 L or greater, usable with biological materials II.A2.014.e. 2B350 2B352 V.A2.007 Fermenters with an internal volume of 10-20 L (0,01-0,02 m3), usable with biological materials 2B352 II.A2.014.a.

V.A6. SENSORS AND LASERS No Description Related item from Annex I to Regulation (EC) No 428/2009 V.A6.001 High-speed imaging cameras except those used in medical imaging systems 6A003.a.2

V.A9. AEROSPACE AND PROPULSION No Description Related item from Annex I to Regulation (EC) No 428/2009 V.A9.001 Non-destructive test chambers with a 1m or more critical internal dimension. 9B106 V.A9.002 Turbo-pumps for liquid or hybrid rocket engines 9A006 V.A9.003 Countermeasure Subsystems and Penetration Aids (e.g. jammers, chaff, decoys) designed to saturate, confuse, or evade missile defences. N/A V.A9.004 Truck chassis with 6 or more axles 9A115 II.A9.003

SOFTWARE No Description Related item from Annex I to Regulation (EC) No 428/2009 V.B.001 Modelling and design software related to the modelling of aerodynamic and thermodynamic analysis of rocket or unmanned aerial vehicle systems. N/A

PART VI

Weapons of mass destruction-related items, materials, equipment, goods and technology identified and designated pursuant to paragraph 4 of UNSCR 2371 (2017).

GOODS

VI.A1. SPECIAL MATERIALS AND RELATED EQUIPMENT No Description Related item from Annex I to Regulation (EC) No 428/2009 VI.A1.001 Explosive bolts, nuts and shackles, flexible linear-shaped charges, ball locks, compression springs, circular cutting devices and acceleration rockets usable for staging mechanisms N/A VI.A1.002 All environmental test chambers capable of simulating flight conditions (temperature, pressure, shock and vibration) except those used for civilian aircraft safety purposes 9B106 VI.A1.003 Rapid prototyping, including additive manufacturing equipment N/A VI.A1.004 Polyacrylonitrile (PAN) fibre usable as a precursor for carbon fibre production and its associated production equipment 1C010 1C210 9C110 VI.A1.005 For point 12 of the list in the report of the Committee prepared in accordance with paragraph 25 of resolution 2270 (2016) (S/2016/308, annex) read Metal hydrides, such as zirconium hydride, beryllium hydride, aluminium hydride, lithium aluminium hydride and titanium hydride 1C111 VI.A1.006 Plasticizers usable in composite propellants, such as 1C111 VI.A1.007 Maraging steel capable of an ultimate tensile strength of 1950 MPa or more at 293 K (20 °C) and in any of the following forms: 1C216 VI.A1.008 Filament winding machines and related equipment: Filament winding machines or fibre/tow-placement machines, of which the motions for positioning, wrapping and winding fibres can be coordinated and programmed in two or more axes and which are designed to fabricate composite structures or laminates from fibrous or filamentary materials, coordinating and programming controls and precision mandrels for such equipment 1B001 1B101 1B201 VI.A1.009 Full face-mask air-purifying and air-supplying respirators except those used in breathing apparatus for firefighters 1A004.a. 2B352 VI.A1.010 Additional chemicals suitable for decontamination of chemical warfare agents: Diethylenetriamine (CAS 111-40-0) N/A VI.A1.011 Nerve agent chemoprophylaxis: N/A

dioctyl adipate (DOA) (CAS 123-79-5)

dioctyl sebacate (DOS) (CAS 122-62-3)

dioctyl azelate (DOZ) (CAS 103-24-2)

VI.A1.

(a) Sheet, plate or tubing with a wall or plate thickness equal to or less than 5,0 mm;

(b) Tubular forms with a wall thickness of 50 mm or less and having an inner diameter of 270 mm or more

Butyrylcholinesterase (BCHE)

Pyridostigmine bromide (CAS 101-26-8)

Obidoxime chloride (CAS 114-90-9)

PART VII

Conventional arms-related items, materials, equipment, goods and technology designated, pursuant to paragraph 5 of UNSCR 2371 (2017).

GOODS

VII.A1. Note: Note: Notes: 1.2. Notes: 1.2.3.4.

SPECIAL MATERIALS AND RELATED EQUIPMENT No Description Related item from Annex I to Regulation (EC) No 428/2009 VII.A1.001 Composite structures or laminates consisting of an organic matrix and materials as follows: Does not apply to 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: Does not apply to semi-finished items, specially designed for purely civilian applications as follows: sporting goods, automotive industry, machine tool industry, medical applications. Does not apply to finished items specially designed for a specific application. 1A002 1A202 VII.A1.002 Fibrous or filamentary materials having any of the following: 1C008 1C010 1C210 9C110 VII.A1.003 1B001.a. 1B001.b. 1B001.c. 1B001.d. 1B001.e. 1B001 1B101 1B201 VII.A1.004 Metal alloys, metal alloy powder and alloyed materials including the following: Unless provision to the contrary is made, the words metals and alloys cover crude and semi-fabricated forms. Crude forms: anodes, balls, bars (including notched bars and wire bars), billets, blocks, blooms, brickets, cakes, cathodes, crystals, cubes, dice, grains, granules, ingots, lumps, pellets, pigs, powder, rondelles, shot, slabs, slugs, sponge, sticks. Semi-fabricated forms: Wrought or worked materials fabricated by rolling, drawing, extruding, forging, impact extruding, pressing, graining, atomising, and grinding, i.e.: angles, channels, circles, discs, dust, flakes, foils and leaf, forging, plate, powder, pressings and stampings, ribbons, rings, rods (including bare welding rods, wire rods, and rolled wire), sections, shapes, sheets, strip, pipe and tubes (including tube rounds, squares, and hollows), drawn or extruded wire. Cast material produced by casting in sand, die, metal, plaster or other types of moulds, including high pressure castings, sintered forms, and forms made by powder metallurgy. 1C002 1C202 VII.A1.005 Magnetic metals, of all types and of whatever form, having any of the following: 1C003 VII.A1.006 Uranium titanium alloys or tungsten alloys with a matrix based on iron, nickel or copper, having all of the following: 1C004 VII.A1.007 Superconductive composite conductors in lengths exceeding 100 m or with a mass exceeding 100 g, as follows: 1C005 VII.A1.008 Fluids and lubricating materials, as follows: Note: Does not apply to materials specified and packages as medical products 1C006 VII.A1.009 Ceramic powders, non-composite ceramic materials, ceramic-matrix composite materials and precursor materials, as follows: Does not apply to abrasives. Does not apply to 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 per cent creep strain at 100 MPa load and 1273 K (1000 °C) for 100 hours. 1C007 VII.A1.010 Non-fluorinated polymeric substances as follows: Note: Applies to the substances in liquid or solid fusible form, including resin, powder, pellet, film, sheet, tape, or ribbon. 1C008 VII.A1.011 Unprocessed fluorinated compounds as follows: 1C009 VII.A1.012 Fibrous or filamentary materials as follows: Does not apply to polyethylene. Does not apply to fibrous or filamentary materials, for the repair of civil aircraft structures or laminates, having all of the following: Does not apply to the following: Does not apply to: 1C010.a. 1C010.b. 1C010.c. VII.A1.013 Metals and compounds, as follows: Note: The metals referred to here also refer to metals or alloys encapsulated in aluminium, magnesium, zirconium or beryllium. 1C011 VII.A1.014 Body armour and components therefor, as follows: Note: this paragraph does not apply to body armour when accompanying its user for the user's own personal protection, to body armour designed to provide frontal protection only from both fragment and blast from non-military explosive devices, and to body armour designed to provide protection only from knife, spike, needle or blunt trauma. 1A005

An area not exceeding 1 m2;

A length not exceeding 2,5 m;

A width exceeding 15 mm.

VII.A1. Note:

(a) Inorganic fibrous or filamentary materials that have a specific modulus exceeding 2,54 × 106 m and a melting, softening, decomposition or sublimation point exceeding 1649 °C in an inert environment. Note: Does not apply to the following

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

Molybdenum and molybdenum alloy fibres

Boron fibres

Discontinuous ceramic fibres with a melting, softening, decomposition or sublimation point lower than 1770 °C in an inert environment.

(b) Notes: 1.2.3.

Fibrous or filamentary materials having any of the following: Does not apply to polyethylene. Does not apply to Does not apply to 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; molybdenum and molybdenum alloy fibres; boron fibres; discontinuous ceramic fibres with a melting, softening, decomposition or sublimation point lower than 1770 °C in an inert environment.

(b)

1. Materials composed of aromatic polyetherimides having a glass transition temperature (Tg) exceeding 290 °C,

2. Polyarylene ketones,

3. Polyarylene sulphides where the arlylene group is biphenylene, triphenylene or combinations thereof,

4. Polybiphenylenethersulphone having a Tg exceeding 290 °C, or

5. Any of the above materials commingled with any of the following:

5. a.

Organic fibrous or filamentary materials, with a specific modulus exceeding 12,7 × 106 m and a specific tensile strength exceeding 23,5 × 104 m.

Carbon fibrous or filamentary materials, having a specific modulus exceeding 14,65 × 106 m; and specific tensile strength exceeding 26,82 × 104 m.

Inorganic fibrous or filamentary materials, having a specific modulus exceeding 2,54 × 106 m; and a melting, softening, decomposition or sublimation point exceeding 1649 °C in an inert environment.

fibrous or filamentary materials, for the repair of civil aircraft structures or laminates, having an area not exceeding 1 m2; a length not exceeding 2,5 m; and a width exceeding 15 mm.

Mechanically chopped, milled or cut carbon fibrous or filamentary materials 25,0 mm or less in length.

(c) Organic fibrous or filamentary materials with a specific modulus exceeding 12,7 × 106 m and with a specific tensile strength exceeding 23,5 × 104 m.

(d) Carbon fibrous or filamentary materials having a specific modulus exceeding 14,65 × 106 m and a specific tensile exceeding 26,82 × 104 m.

(e) Note:

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 any of the following fibrous or filamentary materials and resins: Does not apply to

(e)

1. Inorganic fibrous or filamentary materials with a specific modulus exceeding 2,54 × 106 m and a melting, softening, decomposition or sublimation point exceeding 1649 °C in an inert environment, or

2. Organic or carbon fibrous or filamentary materials, having all of the following:

2. a.

Specific modulus exceeding 10,15 × 106 m; and

Specific tensile strength exceeding 17,7 × 104 m; or

3. Resin or pitch, from unprocessed fluorinated compounds such as:

3. a.

Fluorinated polyimides containing 10 % by weight or more of combined fluorine;

Fluorinated phosphazene elastomers containing 30 % by weight or more of combined fluorine; or

4. Phenolic resins with Dynamic Mechanical Analysis glass transition temperature (DMA Tg) equal to, or exceeding, 180 °C and having a phenolic resin; or

5. Other resin or pitch with Dynamic Mechanical Analysis glass transition temperature (DMA Tg) equal to, or exceeding, 232 °C.

Epoxy resin matrix impregnated carbon fibrous or filamentary materials (prepregs) for the repair of civil aircraft structures or laminates, having all of the following;

An area not exceeding 1 m2;

A length not exceeding 2,5 m; and

A width exceeding 15 mm

(a) Materials composed of aromatic polyetherimides having a glass transition temperature (Tg) exceeding 290 °C.

(b) Polyarylene ketones.

(d) Polybiphenylenethersulphone having a Tg exceeding 290 °C, or

(e) Notes: 1.2.3.

Any of the above materials commingled with any of the following: Does not apply to polyethylene. Does not apply to: Does not apply to 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; molybdenum and molybdenum alloy fibres; boron fibres; discontinuous ceramic fibres with a melting, softening, decomposition or sublimation point lower than 1770 °C in an inert environment

(e)

1. Organic fibrous or filamentary materials, with a specific modulus exceeding 12,7 × 106 m and specific tensile strength exceeding 23,5 × 104 m,

2. Carbon fibrous or filamentary materials, having a specific modulus exceeding 14,65 × 106 m and specific tensile strength exceeding 26,82 × 104 m,

3. Inorganic fibrous or filamentary materials, having a specific modulus exceeding 2,54 × 106 m and melting, softening, decomposition or sublimation point exceeding 1649 °C in an inert environment.

fibrous or filamentary materials, for the repair of civil aircraft structures or laminates, having an area not exceeding 1 m2; a length not exceeding 2,5 m; and a width exceeding 15 mm.

Mechanically chopped, milled or cut carbon fibrous or filamentary materials 25,0 mm or less in length.

Equipment for the production or inspection of composite structures Notes: 1.2.

Specially designed components and accessories to include: For the purposes of this 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. The technique of interlacing includes knitting.

Equipment for the production or inspection of composite structures

(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.

(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.

(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.

(d) Equipment specially designed or adapted for the production of reinforcement fibres, as follows:

(d)

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;

2. Equipment for the chemical vapor deposition of elements or compounds, on heated filamentary substrates, to manufacture silicon carbide fibres;

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;

5. Equipment for producing prepregs specified in VII.A1.003, paragraph d, under Materials, by the hot melt method;

6. Non-destructive inspection equipment specially designed for composite materials, as follows:

6. a.

X-ray tomography systems for three dimensional defect inspection;

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.

(a) Aluminides, including:

(a)

1. Nickel aluminides containing a minimum of 15 % by weight aluminium, a maximum of 38 % by weight aluminium and at least one additional alloying element;

2. Titanium aluminides containing 10 % by weight or more aluminium and at least one additional alloying element.

(b) Metal alloys made from the powder or particulate material including:

(b)

1. Nickel alloys having a stress-rupture life of 10000 hours or longer at 650 °C at a stress of 676 MPa or a low cycle fatigue life of 10000 cycles or more at 550 °C at a maximum stress of 1095 MPa;

2. Niobium alloys having a stress-rupture life of 10000 hours or longer at 800 °C at a stress of 400 MPa or a low cycle fatigue life of 10000 cycles or more at 700 °C at a maximum stress of 700 MPa;

3. Titanium alloys having a stress-rupture life' of 10000 hours or longer at 450 °C at a stress of 200 MPa or a low cycle fatigue life of 10000 cycles or more at 450 °C at a maximum stress of 400 MPa;

4. Aluminium alloys having a tensile strength of 240 MPa or more at 200 °C or a tensile strength of 415 MPa or more at 25 °C;

5. Magnesium alloys having a tensile strength of 345 MPa or more and a corrosion rate of less than 1 mm/year in 3 % sodium chloride aqueous solution measured in accordance with ASTM standard G-31 or national equivalents;

6. Metal alloy powder or particulate material, having all of the following and made from any of the following composition systems:

6. a.

Nickel alloys (Ni-Al-X, Ni-X-Al) qualified for turbine engine parts or components, i.e. with less than 3 non-metallic particles (introduced during the manufacturing process) larger than 100 μm in 109 alloy particles

Niobium alloys (Nb-Al-X or Nb-X-Al, Nb-Si-X or Nb-X-Si, Nb Ti X or Nb-X-Ti)

Titanium alloys (Ti-Al-X or Ti-X-Al)

Aluminium alloys (Al-Mg-X or Al-X-Mg, Al-Zn-X or Al-X-Zn, Al Fe-X or Al-X-Fe) or

Magnesium alloys (Mg-Al-X or Mg-X-Al)

7. Made in a controlled environment by any of the following processes:

7. a.

Vacuum atomization

Gas atomization

Rotary atomization

Splat quenching

Melt spinning and comminution

VII.A1. Note: Note:

(a) Initial relative permeability of 120000 or more and a thickness of 0,5 mm or less

(b) Magnetostrictive alloys having any of the following:

(b)

1. A saturation magnetostriction of more than 5 × 10– 4; or

2. A magnetomechanical coupling factor (k) of more than 0,8; or

(c)

1. A composition having a minimum of 75 % by weight of iron, cobalt or nickel;

2. A saturation magnetic induction (Bs) of 1,6 T or more; and any of the following:

2. a.

A strip thickness of 0,02 mm or less; or

An electrical resistivity of 2 × 10– 4 ohm cm or more.

(a) A density exceeding 17,5 g/cm3;

(b) An elastic limit exceeding 880 MPa;

(d) An elongation exceeding 8 %.

(a) Superconductive composite conductors containing one or more niobium-titanium filaments, having all of the following:

(a)

1. Embedded in a matrix other than a copper or copper-based mixed matrix; and

2. Having a cross-section area less than 0,28x 10– 4 mm2 (6 μm in diameter for circular filaments);

(b) Superconductive composite conductors consisting of one or more superconductive filaments other than niobium-titanium, having all of the following:

(b)

1. A critical temperature at zero magnetic induction exceeding – 263,31 °C; and

2. Remaining in the superconductive state at a temperature of – 268,96 °C when exposed to a magnetic field oriented in any direction perpendicular to the longitudinal axis of conductor and corresponding to a magnetic induction of 12 T with critical current density exceeding 1750 A/mm2 on overall cross-section of the conductor.

(c) Superconductive composite conductors consisting of one or more superconductive filaments, which remain superconductive above – 158,16 °C

(a) Lubricating materials containing, as their principal ingredients, any of the following:

(a)

1. Phenylene or alkylphenylene ethers or thio-ethers, or their mixtures, containing more than two ether or thio-ether functions or mixtures thereof; or

2. Fluorinated silicone fluids with a kinematic viscosity of less than 5000 mm2/s (5000 centistokes) measured at 25 °C;

(b) Damping or flotation fluids having all of the following:

(b)

1. Purity exceeding 99,8 %;

2. Containing less than 25 particles of 200 μm or larger in size per

3. 100 ml; and

4. Made from at least 85 % of any of the following:

4. a.

Dibromotetrafluoroethane (CAS 25497-30-7, 124-73-2, 27336-23-8);

Polychlorotrifluoroethylene (oily and waxy modifications only); or

Polybromotrifluoroethylene

(c)

1. Containing 85 % by weight or more of any of the following, or mixtures thereof:

1. a.

Monomeric forms of perfluoropolyalkylether-triazines or perfluoroaliphatic-ethers;

Perfluoroalkylamines;

Perfluorocycloalkanes; or

Perfluoroalkanes

Density at 298 K (25 °C) of 1,5 g/ml or more;

In a liquid state at 273 K (0 °C); and

Containing 60 % or more by weight of fluorine

(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;

(c) Ceramic-ceramic composite materials with a glass or oxide-matrix and reinforced with fibres having all of the following:

(c)

1. Made from any of the following materials:

1. a.

Si-N;

Si-C;

Si-A1-O-N; or

Si-O-N; and

2. Having a specific tensile strength exceeding 12,7 × 103 m

(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 above, as follows:

(e)

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:

(f)

1. Al2O3 (CAS 1344-28-1); or

2. Si-C-N.

VII.A1. Note: Note: Notes: 1.2.

(a) Imides as follows:

(a)

1. Bismaleimides;

2. Aromatic polyamide-imides (PAI) having a glass transition temperature (Tg) exceeding 290 °C;

3. Aromatic polyimides having a glass transition temperature (Tg) exceeding 232 °C;

4. Aromatic polyetherimides having a glass transition temperature (Tg) exceeding 290°C;

(b) Polyarylene ketones;

(d) Polybiphenylenethersulphone having a glass transition temperature (Tg) exceeding 290°C.

(a) Fluorinated polyimides containing 10 % by weight or more of combined fluorine;

(b) Fluorinated phosphazene elastomers containing 30 % by weight or more of combined fluorine.

(a) Organic fibrous or filamentary materials, having all of the following:

(a)

1. specific modulus exceeding 12,7 × 106 m; and

2. specific tensile strength exceeding 23,5 × 104 m;

(b) Carbon fibrous or filamentary materials, having all of the following:

(b)

1. specific modulus exceeding 14,65 × 106 m; and

2. specific tensile strength exceeding 26,82 × 104 m;

(c)

1. Specific modulus exceeding 2,54 × 106 m; and

2. Melting, softening, decomposition or sublimation point exceeding 1649 °C in an inert environment

(d) Fibrous or filamentary materials, having any of the following:

(d)

1. Composed of any of the following:

1. a.

Polyetherimides specified in VII.A1.010

Other materials specified in VII.A1.010

2. Composed of materials specified above and commingled with other fibres specified in VII.A1.012.

(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:

(e)

1. Having any of the following:

1. a.

Inorganic fibrous or filamentary materials specified above

Organic or carbon fibrous or filamentary materials, having all of the following:

1. Specific modulus exceeding 10,15 × 106 m; and

2. Specific tensile strength exceeding 17,7 × 104 m; and

2. Having any of the following:

2. a.

Resin or pitch, specified in previous sections;

Dynamic Mechanical Analysis glass transition temperature (DMA Tg) equal to or exceeding 180 °C and having a phenolic resin; or

Dynamic Mechanical Analysis glass transition temperature (DMA Tg) equal to or exceeding 232 °C and having a resin or pitch, not specified earlier and not being a phenolic resin.

VII.A1. Note: Note: Notes: 1.2. Notes: 1.2.

(a) An area not exceeding 1 m2;

(b) A length not exceeding 2,5 m; and

(c) A width exceeding 15 mm. Or to mechanically chopped, milled or cut carbon fibrous or filamentary materials 25,0 mm or less in length.

VII.A1. Note: Note: Notes: 1.2. Notes: 1.2.3.

(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;

(d) Discontinuous ceramic fibres with a melting, softening, decomposition or sublimation point lower than 2043 K (1770 °C) in an inert environment.

VII.A1. Note: Note: Notes: 1.2. Notes: 1.2.3.4.

(a) Epoxy resin matrix impregnated carbon fibrous or filamentary materials (prepregs) for the repair of civil aircraft structures or laminates, having all of the following;

(a)

1. An area not exceeding 1 m2;

2. A length not exceeding 2,5 m; and

3. 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 previously.

(a) Metals in particle sizes of less than 60 μm whether spherical, atomized, spheroidal, flaked or ground, manufactured from material consisting of 99 % or more of zirconium, magnesium and alloys thereof;

(b) Boron or boron alloys, with a particle size of 60 μm or less, as follows:

(b)

1. Boron with a purity of 85 % by weight or more;

2. Boron alloys with a boron content of 85 % by weight or more;

(d) Nitroguanidine (NQ) (CAS 556-88-7)

(a) Soft body armour not manufactured to military standards or specifications, or to their equivalents, and specially designed components therefor;

(b) Hard body armour plates providing ballistic protection equal to or less than level IIIA (NIJ 0101.06, July 2008) or national equivalents.

VII.A4. COMPUTERS No Description Related item from Annex I to Regulation (EC) No 428/2009 VII.A4.001 Electronic computers and related systems, equipment and components, or electronic assemblies having any of the following: 4A001

VII.A4.

(a) Specially designed to have any of the following:

(a)

1. Radiation hardened to exceed any of the following specifications:

1. a.

Total dose 5 × 103 Gy (Si);

Dose rate upset 5 × 106 Gy (Si)/s; or

Single event upset 1 × 10– 8 error/bit/day.

VII.A5. TELECOMUNICATIONS AND INFORMATION SECURITY No Description Related item from Annex I to Regulation (EC) No 428/2009 VII.A5.001 Telecommunication systems and equipment, and specially designed components and accessories therefor, having any of the following characteristics, functions or features: 5A001.b. VII.A5.002 Telecommunication test, inspection and production equipment and specially designed components or accessories therefor, specially designed for the development or production of telecommunication equipment, functions or features. Note: Does not apply to optical fibre characterization equipment. 5B002

VII.A5.

(a) Specially designed to have any of the following: Note: Does not apply to radio equipment specially designed for use with any of the following:

(a)

1. User programmable spreading codes; or

2. A total transmitted bandwidth which is 100 or more times the bandwidth of any one information channel and in excess of 50 kHz.

(a) Civil cellular radio-communications systems; or

(b) Fixed or mobile satellite earth stations for commercial civil telecommunications.

(b) Technical note:

Being digitally controlled radio receivers having all of the following: Note: Does not apply to radio equipment specially designed for use with civil cellular radio-communications systems. Channel switching time: the time (i.e., delay) to change from one receiving frequency to another, to arrive at or within ± 0,05 % of the final specified receiving frequency. Items having a specified frequency range of less than ± 0,05 % around their centre frequency are defined to be incapable of channel frequency switching.

(b)

1. More than 1000 channels;

2. A channel switching time of less than 1 ms;

3. Automatic searching or scanning of a part of the electromagnetic spectrum; and

4. Identification of the received signals or the type of transmitter.

VII.A6 Technical note: Notes: 1.2. Note:

SENSORS AND LASERS No Description Related item from Annex I to Regulation (EC) No 428/2009 VII.A6.001 Hydrophones having any of the following: Note: The status of hydrophones specially designed for other equipment is determined by the status of the other equipment. 6A001.a. VII.A6.002 Towed acoustic hydrophone arrays having any of the following: 6A001.a. VII.A6.003 Heading sensors having all of the following: 6A001.a. VII.A6.004 Bottom or bay-cable hydrophone arrays having any of the following: Accelerometer-based hydro-acoustic sensors having all of the following: Does not apply to particle velocity sensors or geophones. Also applies to receiving equipment, whether or not related in normal application to separate active equipment, and specially designed components therefor. 6A001.a. VII.A6.005 Monospectral imaging sensors and multispectral imaging sensors, designed for remote sensing applications and having any of the following: Note: Does not apply to monospectral imaging sensors' with a peak response in the wavelength range exceeding 300 nm but not exceeding 900 nm and only incorporating any of the following non space-qualified detectors or non-space-qualified focal plane arrays: 6A002 VII.A6.006 Space-qualified components for optical systems, as follows: 6A004.a. VII.A6.007 Optical control equipment as follows: 6A004.d. VII.A6.008 Magnetometers using superconductive technology (SQUID) and having any of the following: 6A006 Except: VII.A6.009 Magnetometers using optically pumped or nuclear precession (proton/Overhauser) technology having a sensitivity lower (better) than 2 pT (rms) per square root Hz at a frequency of 1 Hz; 6A006 VII.A6.010 Magnetic gradiometers using multiple magnetometers specified in VII.A6; 6A006 VII.A6.011 Compensation systems for the following: Fibre optic intrinsic magnetic gradiometers having a magnetic gradient field sensitivity lower (better) than 0,3 nT/m (rms) per square root Hz; 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. 6A006 VII.A6.012 Underwater electromagnetic receivers incorporating magnetometer specified by section 1 or 2 Magnetic and electric field sensors. 6A006

VII.A6

(a) Incorporating continuous flexible sensing elements

(b) Incorporating flexible assemblies of discrete sensing elements with either a diameter or length less than 20 mm and with a separation between elements of less than 20 mm;

(c)

1. Optical fibres;

2. Piezoelectric polymer films other than polyvinylidene-fluoride (PVDF) and its co-polymers {P(VDF-TrFE) and P(VDF-TFE)};

3. Flexible piezoelectric composites

4. Lead-magnesium-niobate/lead-titanate (i.e., Pb(Mg 1/3 Nb 2/3)O3-PbTiO3, or PMN-PT) piezoelectric single crystals grown from solid solution; or

5. Lead-indium-niobate/lead-magnesium niobate/lead-titanate (i.e., Pb(In1/2 Nb1/2)O3–Pb(Mg1/3 Nb2/3)O3–PbTiO3, or PIN-PMN-PT) piezoelectric single crystals grown from solid solution;

(d) Designed to operate at depths exceeding 35 m with acceleration compensation; or

(e) Designed for operation at depths exceeding 1000 m.

(a) Hydrophone group spacing of less than 12,5 m or able to be modified to have hydrophone group spacing of less than 12,5 m;

(b) Designed or able to be modified to operate at depths exceeding 35 m;

(d) Longitudinally reinforced array hoses;

(e) An assembled array of less than 40 mm in diameter;

(f) Hydrophone characteristics specified in (a) above or a hydrophone with a hydrophone sensitivity better than 180 dB at any depth with no acceleration, or

(g) Accelerometer-based hydro-acoustic with the following:

(g)

1. Composed of three accelerometers arranged along three distinct axes;

2. Having an overall acceleration sensitivity better than 48 dB (reference 1000 mV rms per 1g);

3. Designed to operate at depths greater than 35 metres; and

4. Operating frequency below 20 kHz.

(a) An accuracy of better than 0,5°; and

(b) Designed to operate at depths exceeding 35 m or having an adjustable or removable depth sensing device in order to operate at depths exceeding 35 m;

(a) Incorporating hydrophones specified in VII.A6.002 or a hydrophone with a hydrophone sensitivity better than 180 dB at any depth with no acceleration.

(b) Incorporating multiplexed hydrophone group signal modules having all of the following characteristics:

(b)

1. Designed to operate at depths exceeding 35 m or having an adjustable or removable depth sensing device in order to operate at depths exceeding 35 m; and

2. Capable of being operationally interchanged with towed acoustic hydrophone array modules; or

VII.A6 Technical note:

1. Composed of three accelerometers arranged along three distinct axes;

2. Having an overall acceleration sensitivity better than 48 dB (reference 1000 mV rms per 1g);

3. Designed to operate at depths greater than 35 metres; and

4. Operating frequency below 20 kHz.

VII.A6 Technical note: Notes: 1.2.

(a) An Instantaneous-Field-Of-View (IFOV) of less than 200 μrad (microradians); or

(b) Specified for operation in the wavelength range exceeding 400 nm but not exceeding 30000 nm and having all the following;

(b)

1. Providing output imaging data in digital format; and

2. Having any of the following characteristics:

2. a.

Space-qualified; or

Designed for airborne operation, using other than silicon detectors, and having an IFOV of less than 2,5 mrad (milliradians);

(a) Charge Coupled Devices not designed or modified to achieve charge multiplication; or

(b) Complementary Metal Oxide Semiconductor devices not designed or modified to achieve charge multiplication.

(a) Components lightweighted to less than 20 % equivalent density compared with a solid blank of the same aperture and thickness;

(b) Raw substrates, processed substrates having surface coatings (single-layer or multi-layer, metallic or dielectric, conducting, semiconducting or insulating) or having protective films;

(c) Segments or assemblies of mirrors designed to be assembled in space into an optical system with a collecting aperture equivalent to or larger than a single optic 1 m in diameter;

(d) Components manufactured from composite materials having a coefficient of linear thermal expansion equal to or less than 5 × 10– 6 in any coordinate direction;

(a) Equipment specially designed to maintain the surface figure or orientation of the space-qualified components specified above.

(b) Steering, tracking, stabilization and resonator alignment equipment as follows:

(b)

1. Beam steering mirror stages designed to carry mirrors having diameter or major axis length greater than 50 mm and having all of the following, and specially designed electronic control equipment therefor:

1. a.

A maximum angular travel of ±26 mrad or more;

A mechanical resonant frequency of 500 Hz or more; and

An angular accuracy of 10 μrad (microradians) or less (better);

2. Resonator alignment equipment having bandwidths equal to or more than 100 Hz and an accuracy of 10 μrad or less (better);

(c)

1. A maximum slew exceeding 5°;

2. A bandwidth of 100 Hz or more;

3. Angular pointing errors of 200 μrad (microradians) or less; and

4. Having any of the following:

4. a.

Exceeding 0,15 m but not exceeding 1 m in diameter or major axis length and capable of angular accelerations exceeding 2 rad (radians)/s2; or

Exceeding 1 m in diameter or major axis length and capable of angular accelerations exceeding 0,5 rad (radians)/s2.

(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; or

(b) SQUID systems having an in-motion-magnetometer sensitivity lower (better) than 2 pT (rms) per square root Hz at a frequency of 1 Hz and specially designed to reduce in-

6A006.a.3 "Magnetometers" using fluxgate "technology"

6A006.a.4 Induction coil "magnetometers"

6A006.b. Underwater electric field sensors

(a) 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, and using optically pumped or nuclear precession (proton/Overhauser) technology that will permit these sensors to realize a sensitivity lower (better) than 2 pT rms per square root Hz.

(b) Underwater electric field sensors having a sensitivity lower (better) than 8 nanovolt per meter per square root Hz when measured at 1 Hz.

(c) Magnetic gradiometers specified in VII.A6.010 that will permit these sensors to realize a sensitivity lower (better) than 3 pT/m rms per square root H

VII.A7. Notes: 1.2.

NAVIGATION AND AVIONICS No Description Related item from Annex I to Regulation (EC) No 428/2009 VII.A7.001 Accelerometers as follows and specially designed components therefor: 7A001 VII.A7.002 Gyros or angular rate sensors, having any of the following and specially designed components therefor: 7A002 VII.A7.003 Inertial measurement equipment or systems, having any of the following: 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: This paragraph does not apply to inertial measurement equipment or systems which are certified for use on civil aircraft by civil aviation authorities of one or more Member States. 7A003

VII.A7.

(a) Linear accelerometers having any of the following: Note: paragraphs above do not apply to accelerometers limited to measurement of only vibration or shock.

(a)

1. Specified to function at linear acceleration levels less than or equal to 15 g and having any of the following:

1. a.

A bias stability of less (better) than 130 micro g with respect to a fixed calibration value over a period of one year; or

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:

2. a.

A bias repeatability of less (better) than 1250 micro g over a period of one year; and

A scale factor repeatability of less (better) than 1250 ppm over a period of one year; or

3. Designed for use in inertial navigation or guidance systems and specified to function at linear acceleration levels exceeding 100 g;

(b) Angular or rotational accelerometers, specified to function at linear acceleration levels exceeding 100 g.

(a) Specified to function at linear acceleration levels less than or equal to 100 g and having any of the following:

(a)

1. A rate range of less than 500 degrees per second and having any of the following: Note: this paragraph does not apply to spinning mass gyros.

1. 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; or

An angle random walk of less (better) than or equal to 0,0035 degree per square root hour; or

2. A rate range greater than or equal to 500 degrees per second and having any of the following: Note: this paragraph does not apply to spinning mass gyros.

2. 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; or

An angle random walk of less (better) than or equal to 0,1 degree per square root hour; or

(b) Specified to function at linear acceleration levels exceeding 100 g.

Attitude and Heading Reference Systems (AHRSs);

Gyrocompasses;

Inertial Measurement Units (IMUs);

Inertial Navigation Systems (INSs);

Inertial Reference Systems (IRSs);

Inertial Reference Units (IRUs).

VII.A7. Notes: 1.2.

(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:

(a)

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); or

3. Total drift of 1 nautical mile CEP or less (better) in a 24 hr period;

(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 metres CEP;

(c) Designed for aircraft, land vehicles or vessels, providing heading or True North determination and having any of the following:

(c)

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); or

2. 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);

(d) Providing acceleration measurements or angular rate measurements, in more than one dimension, and having any of the following:

(d)

1. Performance specified for accelerometers and gyros described above along any axis, without the use of any aiding references; or

2. 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.

VII.A8. MARINE No Description Related item from Annex I to Regulation (EC) No 428/2009 VII.A8.001 Air independent power systems specially designed for underwater use, as follows: 8A002.j. VII.A8.002 Diesel cycle engine air independent systems having all of the following: 8A002.j. VII.A8.003 Fuel cell air independent power systems with an output exceeding 2kW and having any of the following: 8A002.j. VII.A8.004 Stirling cycle engine air independent power systems having all of the following: 8A002.p. VII.A8.005 Manned, tethered submersible vehicles designed to operate at depths exceeding 1000 m. 8A001.a.

VII.A8.

(a) Brayton or Rankine cycle engine air independent power systems having any of the following:

(a)

1. Chemical scrubber or absorber systems, specially designed to remove carbon dioxide, carbon monoxide and particulates from recirculated engine exhaust;

2. Systems specially designed to use a monoatomic gas;

3. Devices or enclosures, specially designed for underwater noise reduction in frequencies below 10 kHz, or special mounting devices for shock mitigation; or

4. Systems having all of the following:

4. a.

Specially designed to pressurise the products of reaction or for fuel reformation;

Specially designed to store the products of the reaction; and

Specially designed to discharge the products of the reaction against a pressure of 100 kPa or more;

(a) Chemical scrubber or absorber systems, specially designed to remove carbon dioxide, carbon monoxide and particulates from recirculated engine exhaust;

(b) Systems specially designed to use a monoatomic gas;

(c) Devices or enclosures, specially designed for underwater noise reduction in frequencies below 10 kHz, or special mounting devices for shock mitigation; and

(d) Specially designed exhaust systems that do not exhaust continuously the products of combustion;

(a) Devices or enclosures, specially designed for underwater noise reduction in frequencies below 10 kHz, or special mounting devices for shock mitigation; or

(b) Systems having all of the following:

(b)

1. Specially designed to pressurise the products of reaction or for fuel reformation;

2. Specially designed to store the products of the reaction; and

3. Specially designed to discharge the products of the reaction against a pressure of 100 kPa or more

(a) Devices or enclosures, specially designed for underwater noise reduction in frequencies below 10 kHz, or special mounting devices for shock mitigation; and

(b) Specially designed exhaust systems which discharge the products of combustion against a pressure of 100 kPa or more;

VII.A9. AEROSPACE AND PROPULSION No Description Related item from Annex I to Regulation (EC) No 428/2009 VII.A9.001 Equipment, tooling or fixtures, specially designed for manufacturing gas turbine engine blades, vanes or tip shrouds, as follows: 9B001 VII.A9.002 Aero gas turbine engines, except aero gas turbine engines which meet all of the following: 9A001

VII.A9.

(a) Directional solidification or single crystal casting equipment;

(b) Casting tooling, manufactured from refractory metals or ceramics, as follows:

(b)

1. Cores

2. Shells (moulds)

3. Combined core and shell (mould) units

(a) Certified by civil aviation authorities of one or more Member States; and

(b) Intended to power non-military manned aircraft for which any of the following has been issued by civil aviation authorities of one or more Member States for the aircraft with this specific engine type:

(b)

1. A civil type certificate; or

2. An equivalent document recognized by the International Civil Aviation Organization.

SOFTWARE No Description Related item from Annex I to Regulation (EC) No 428/2009 VII.B.001 Software for the development of the material listed in VII.A1. 1D002 VII.B.002 Software specially designed for the development or production of equipment as follows: 2D001 2D002 VII.B.003 Software for marine systems, equipment, components, test, inspection and production equipment and other related technology 8D001 8D002

(a) Machine tools for turning having two or more axes which can be coordinated simultaneously for contouring control having any of the following:

(a)

1. Unidirectional positioning repeatability equal to or less (better) than 0,9 μm along one or more linear axis with a travel length less than 1,0 m; or

2. Unidirectional positioning repeatability equal to or less (better) than 1,1 μm along one or more linear axis with a travel length equal to or greater than 1,0 m.

(b) Machine tools for milling having any of the following:

(b)

1. Three linear axes plus one rotary axis which can be coordinated simultaneously for contouring control having any of the following:

1. a.

Unidirectional positioning repeatability equal to or less (better) than 0,9 μm along one or more linear axis with a travel length less than 1,0 m; or

Unidirectional positioning repeatability equal to or less (better) than 1,1 μm along one or more linear axis with a travel length equal to or greater than 1,0 m.

2. Five or more axes which can be coordinated simultaneously for contouring control having any of the following:

2. a.

Unidirectional positioning repeatability equal to or less (better) than 0,9 μm along one or more linear axis with a travel length less than 1,0 m;

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;

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;

3. A unidirectional positioning repeatability for jig boring machines equal to or less (better) than 1,1 μm along one or more linear axis.

4. Electrical discharge machines of the non-wire type which have two or more rotary axes which can be coordinated simultaneously for contouring control.

5. Deep-hole-drilling machines and turning machines modified for deep-hole-drilling, having a maximum depth-of-bore capability exceeding 5 m.

6. Numerically controlled or manual machine tools, and specially designed components, controls and accessories therefor, specially designed for the shaving, finishing, grinding or honing of hardened (Rc = 40 or more) spur, helical and double-helical gears with a pitch diameter exceeding 1250 mm and a face width of 15 % of pitch diameter or larger finished to a quality of AGMA 14 or better (equivalent to ISO 1 328 class 3).

TECHNOLOGY No Description Related item from Annex I to Regulation (EC) No 428/2009 VII.C.001 Technology for the development or production of equipment or materials listed in VII.A 1E001 1E002 1E102 1E103 1E104 1E201 VII.C.002 Technology for the repair of composite structures, laminates or materials specified by the systems, equipment and components listed in VII.A1. Note: Does not apply to technology for the repair of civil aircraft structures using carbon fibrous or filamentary materials and epoxy resins, contained in aircraft manufacturers' manuals. 1E001 1E002 1E201 1E103 VII.C.003 Technology for marine systems, equipment, components, test, inspection and production equipment and other related technology. 8E001 8E002

PART VIII

Weapons of mass destruction-related items, materials, equipment, goods and technology designated, pursuant to paragraph 4 of UNSCR 2375 (2017).

GOODS

VIII.A0. NUCLEAR MATERIALS, FACILITIES, AND EQUIPMENT No Description Related item from Annex I to Regulation (EC) No 428/2009 VIII.A0.001 Ring magnets (except those designed for consumer electronics or automobile applications) 0B001 VIII.A0.002 Hot cells 0B006 VIII.A0.003 Glove boxes suitable for use with radioactive materials 0B005 VIII.A0.004 Electrolytic cells for fluorine production 0B001 VIII.A0.005 Particle accelerators N/A VIII.A0.006 Freon and chilled-water cooling systems capable of continuous cooling capacity of 100000 Btu/hr (29,3 kW) or greater 0B001 0B002 1B231 VIII.A0.007 Bellows-sealed valves 0B001 2A226 VIII.A0.008 Monel equipment, including valves, piping, tanks and vessels (pipes and valves greater than 8-in diameter and rated for 500 psi and tanks greater than 500 l) 0B001 2A226 2B350 VIII.A0.009 Grade 304, 316 and austenitic stainless steel plates, valves, piping, tanks and vessels (pipes and valves greater than 8-in diameter and rated for 500 psi and tanks greater than 500 l) 0B001 1C116 1C216 VIII.A0.010 Vacuum valves, piping, flanges, gaskets and related equipment specially designed for use in high-vacuum service (0,1 Pa or lower pressure) 0B001 0B002 2A226 2B350

VIII.A1. SPECIAL MATERIALS AND RELATED EQUIPMENT No Description Related item from Annex I to Regulation (EC) No 428/2009 VIII.A1.001 Radiation detection, monitoring and measurement equipment 1A004 6A002 6A102 VIII.A1.002 Radiographic detection equipment such as X-ray converters, and storage phosphor image plates (except X-ray equipment specially designed for medical use) 1B001 9B007 VIII.A1.003 Tributyl phosphate (CAS 126-73-8) N/A VIII.A1.004 Nitric acid in concentrations of 20 % of weight or greater 1C111 VIII.A1.005 Fluorine (except that used for strictly civilian purposes, such as refrigerants, including freon and fluoride for toothpaste production) 1C350 VIII.A1.006 Alpha-emitting radionuclides 1C236 VIII.A1.007 Radiation-hardened television cameras 6A003

VIII.A2. MATERIALS PROCESSING No Description Related item from Annex I to Regulation (EC) No 428/2009 VIII.A2.001 Hardened steel and tungsten carbide precision ball bearings (3-mm diameter or greater) 2A001 2A101 VIII.A2.002 Isostatic presses 2B004 2B104 2B204 VIII.A2.003 Electroplating equipment designed for coating parts with nickel or aluminium 2B005 VIII.A2.004 Bellows manufacturing equipment, including hydraulic forming equipment and bellows forming dies 2B009 2B109 2B209 VIII.A2.005 Metal inert gas welders (greater than 180 A DC) N/A VIII.A2.006 Centrifugal multiplane balancing machines 2B119 2B219 VIII.A2.007 Seismic detection equipment or seismic intrusion-detection systems that detect, classify and determine the bearing of the source of a detected signal 2B116 9B006

VIII.A3. ELECTRONICS No Description Related item from Annex I to Regulation (EC) No 428/2009 VIII.A3.001 Frequency changers capable of operating in the frequency range of 300-600 Hz 3A225 VIII.A3.002 Mass spectrometers 3A233 VIII.A3.003 All flash X-ray machines and parts or components of pulsed power systems designed therefrom, including Marx generators, high-power pulse-shaping networks, high-voltage capacitors and triggers 3A102 VIII.A3.004 Electronic equipment of synthesized frequencies within the range of 31,8 GHz or greater and power output of 100 mW or greater for time-delay generation or time-interval measurement, as follows: 3B002 VIII.A3.005 Chromatography and spectrometry analytical instruments 3A233

VIII.A3.

(a) digital time delay generators with a resolution of 50 nanoseconds or less over time intervals of 1 microsecond or greater; or

(b) multichannel (i.e., with 3 or more channels) or modular time interval meters and chronometry equipment with resolution of 50 nanoseconds or less over time intervals of 1 microsecond or greater

SOFTWARE No Description Related item from Annex I to Regulation (EC) No 428/2009 VIII.B.001 Software for neutronic calculations/modelling 0D001 VIII.B.002 Software for radiation transport calculations/modelling 0D001 VIII.B.003 Software for hydrodynamic calculations/modelling (except those used strictly for civilian purposes, such as but not limited to communal heating utilities) 0D001

PART IX

Conventional arms-related items, materials, equipment, goods and technology designated, pursuant to paragraph 5 of UNSCR 2375 (2017).

GOODS

IX.A1. SPECIAL MATERIALS AND RELATED EQUIPMENT No Description Related item from Annex I to Regulation (EC) No 428/2009 IX.A1.001 Seals, gaskets, sealants or fuel bladders, specially designed for aircraft or aerospace use, made from more than 50 % by weight of any of the fluorinated polyimides or fluorinated phosphazene elastomers. 1A001 IX.A1.002 Manufactures of non-fusible aromatic polyimides in film, sheet, tape or ribbon: Note: The category above does not apply to manufactures when coated or laminated with copper and designed for the production of electronic printed circuit boards. 1A003 IX.A1.003 Protective and detection equipment and components, not specially designed for military use, as follows: 1A004.a. Except 1A004.a: riot control agents IX.A1.004 Equipment and devices, specially designed to initiate charges and devices containing energetic materials, by electrical means, as follows: 1A007 IX.A1.005 Charges, devices and components, as follows: 1A008 IX.A1.006 Equipment for the production or inspection of composite structures or laminates or fibrous or filamentary materials as follows, and specially designed components and accessories therefor: 1B001.g. IX.A1.007 Equipment for producing metal alloys, metal alloy powder or alloyed material specially designed to avoid contamination and specially designed for use in one of the following processes: 1B002 IX.A1.008 Tools, dies, moulds or fixtures, for superplastic forming or diffusion bonding titanium, aluminium or their alloys: 1B003 IX.A1.009 Materials specially designed for use as absorbers of electromagnetic waves, or intrinsically conductive polymers, as follows: Technical note: Bulk electrical conductivity and sheet (surface) resistivity should be determined using ASTM D-257 or national equivalents. 1C001.c. IX.A1.010 Superconductive composite conductors consisting of one or more superconductive filaments, which remain superconductive above 115 K (– 158,16 °C). Technical note: For the purposes of the item above, filaments may be in wire, cylinder, film, tape or ribbon form. 1C005.a. IX.A1.011 Fibrous or filamentary materials, as follows: 1C010.a. 1C010.b. 1C010.c.

IX.A1.

(a) A thickness exceeding 0,254 mm; or

(b) Coated or laminated with carbon, graphite, metals or magnetic substances.

(a) Full face masks, filter canisters, protective suits, gloves and shoes, detection systems and decontamination equipment specially designed or modified for defence against any of the following:

(a)

1. Biological agents;

2. Radioactive materials; or

3. Chemical warfare (CW) agents.

(a) Explosive detonator firing sets designed to drive explosive detonators specified in item (b);

(b) Electrically driven explosive detonators, as follows:

(b)

1. Exploding bridge (EB);

2. Exploding bridge wire (EBW);

3. Slapper; or

4. Exploding foil initiators (EFI).

(a) Shaped charges;

(a)

1. Net Explosive Quantity (NEQ) greater than 90 g; and

2. Outer casing diameter equal to or greater than 75 mm;

(b) Linear shaped cutting charges;

(b)

1. An explosive load greater than 40 g/m; and

2. A width of 10 mm or more;

(d) Cutters and severing tools, having a NEQ greater than 3,5 kg, and other severing tools.

(a) 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.

(a) Vacuum atomization;

(b) Gas atomization;

(d) Splat quenching;

(e) Melt spinning and comminution;

(f) Melt extraction and comminution;

(g) Mechanical alloying; or

(h) Plasma atomization.

(a) Airframe or aerospace structures;

(b) Aircraft or aerospace engines; or

(a) 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:

(a)

1. Polyaniline;

2. Polypyrrole;

3. Polythiophene;

4. Poly phenylene-vinylene; or

5. Poly thienylene-vinylene.

(a) Organic fibrous or filamentary materials, having all of the following: Note: This item does not apply to polyethylene.

(a)

1. Specific modulus exceeding 12,7 × 106 m; and

2. Specific tensile strength exceeding 23,5 × 104 m;

(b) Carbon fibrous or filamentary materials, having all of the following:

(b)

1. Specific modulus exceeding 14,65 × 106 m; and

2. Specific tensile strength exceeding 26,82 × 104 m;

(c)

1. Specific modulus exceeding 2,54 × 106 m; and

2. Melting, softening, decomposition or sublimation point exceeding 1922 K (1649 °C) in an inert environment.

IX.A2. MATERIALS PROCESSING No Description Related item from Annex I to Regulation (EC) No 428/2009 IX.A2.001 Anti-friction bearings and bearing systems, as follows, and components therefore: Note: This category does not apply to balls with tolerances specified by the manufacturer in accordance with ISO 3290 as grade 5 or worse. 2A001.a. 2A001.c. IX.A2.002 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: 2B001.c. IX.A2.003 Numerically controlled optical finishing machine tools equipped for selective material removal to produce non-spherical optical surfaces having all of the following characteristics: Technical notes: For the purposes of the items above: 2B002.a. 2B002.b. 2B002.c. 2B002.d. IX.A2.004 Hot isostatic presses having all of the following, and specially designed components and accessories therefor: 2B004 2B104 2B204 IX.A2.005 Equipment specially designed for the deposition, processing and in-process control of inorganic overlays, coatings and surface modifications, as follows: 2B005 IX.A2.006 Dimensional inspection or measuring systems, equipment and electronic assemblies, as follows: 2B006.b. 2B206.b. IX.A2.007 Robots having any of the following characteristics and specially designed controllers and end-effectors therefor: 2B007 2B207 IX.A2.008 Assemblies or units, specially designed for machine tools, or dimensional inspection or measuring systems and equipment, as follows: 2B008 IX.A2.009 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: Technical note: Machines combining the functions of spin-forming and flow-forming are regarded as flow-forming machines. 2B009 2B109 2B209

IX.A2. (a) Technical notes: 1.2.

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, made from monel or beryllium; Ring —annular part of a radial rolling bearing incorporating one or more raceways (ISO 5593:1997). Rolling element —ball or roller which rolls between raceways (ISO 5593:1997).

(b) Active magnetic bearing systems using any of the following:

(b)

1. Materials with flux densities of 2,0 T or greater and yield strengths greater than 414 MPa;

2. All-electromagnetic three-dimensional homopolar bias designs for actuators; or

3. High-temperature (450 K (177 °C) and above) position sensors.

(a) Machine tools for grinding having any of the following:

(a)

1. Three or more axes which can be coordinated simultaneously for contouring control and a unidirectional positioning repeatability equal to or less (better) than 1,1 μm along one or more linear axis; or

2. Five or more axes which can be coordinated simultaneously for contouring control;

(b) Machine tools for removing metals, ceramics or composites, having all of the following:

(b)

1. Removing material by means of any of the following:

1. a.

Water or other liquid jets, including those employing abrasive additives;

Electron beam; or

Laser beam; and

2. At least two rotary axes that can be coordinated simultaneously for contouring control.

(a) Finishing the form to less (better) than 1,0 μm;

(b) Finishing to a roughness less (better) than 100 nm rms;

(d) Using any of the following processes:

(d)

1. Magnetorheological finishing (MRF);

2. Electrorheological finishing (ERF);

3. Energetic particle beam finishing;

4. Inflatable membrane tool finishing; or

5. Fluid jet finishing.

1. MRF is a material removal process using an abrasive magnetic fluid whose viscosity is controlled by a magnetic field.

2. ERF is a removal process using an abrasive fluid whose viscosity is controlled by an electric field.

3. Energetic particle beam finishing uses Reactive Atom Plasmas (RAP) or ion beams to selectively remove material.

4. Inflatable membrane tool finishing is a process that uses a pressurized membrane that deforms to contact the workpiece over a small area

5. Fluid jet finishing makes use of a fluid stream for material removal

(a) A controlled thermal environment within the closed cavity and a chamber cavity with an inside diameter of 406 mm or more; and

(b) Having any of the following:

(b)

1. A maximum working pressure exceeding 207 MPa;

2. A controlled thermal environment exceeding 1773 K (1500 °C); or

3. A facility for hydrocarbon impregnation and removal of resultant gaseous degradation products.

(a) Chemical vapour deposition (CVD) production equipment having all of the following:

(a)

1. A process modified for one of the following:

1. a.

Pulsating CVD;

Controlled nucleation thermal deposition (CNTD); or

Plasma enhanced or plasma assisted CVD; and

2. Having any of the following:

2. a.

Incorporating high vacuum (equal to or less than 0,01 Pa) rotating seals; or

Incorporating in situ coating thickness control;

(b) Ion implantation production equipment having beam currents of 5 mA or more;

(c) Electron beam physical vapour deposition (EB-PVD) production equipment incorporating power systems rated for over 80 kW and having any of the following:

(c)

1. A liquid pool level laser control system which regulates precisely the ingots feed rate; or

2. A computer controlled rate monitor operating on the principle of photo-luminescence of the ionized atoms in the evaporant stream to control the deposition rate of a coating containing two or more elements;

(d) Plasma spraying production equipment having any of the following:

(d)

1. Operating at reduced pressure controlled atmosphere (equal to or less than 10 kPa measured above and within 300 mm of the gun nozzle exit) in a vacuum chamber capable of evacuation down to 0,01 Pa prior to the spraying process; or

2. Incorporating in situ coating thickness control;

(e) Sputter deposition production equipment capable of current densities of 0,1 mA/mm2 or higher at a deposition rate of 15 μm/h or more;

(f) Cathodic arc deposition production equipment incorporating a grid of electromagnets for steering control of the arc spot on the cathode; or

(g) Ion plating production equipment capable of in situ measurement of any of the following:

(g)

1. Coating thickness on the substrate and rate control; or

2. Optical characteristics.

(a) Computer-controlled or numerically controlled Coordinate Measuring Machines (CMM), having a three-dimensional (volumetric) maximum permissible error of length measurement (E0,MPE) at any point within the operating range of the machine (i.e., within the length of axes) equal to or less (better) than 1,7 + L/1000 μm (L is the measured length in mm), according to ISO 10360-2 (2009);

(b) Linear and angular displacement measuring instruments, as follows: Note: The category above does not apply to optical instruments, such as autocollimators, using collimated light (e.g., laser light) to detect angular displacement of a mirror.

(b)

1. Linear displacement measuring instruments having any of the following:

1. 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. Technical note:

Linear Variable Differential Transformer (LVDT) systems: For the purposes of item b. above, 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.

1. Having any of the following:

1. 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; or

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; and

2. Drift equal to or less (better) than 0,1 % per day at a standard ambient test room temperature ± 1 K;

Measuring systems having all of the following:

1. Containing a laser;

2. A resolution over their full scale of 0,200 nm or less (better); and

3. Capable of achieving a measurement uncertainty equal to or less (better) than (1,6 + L/2000) nm (L is the measured length in mm) at any point within a measuring range, when compensated for the refractive index of air and measured over a period of 30 seconds at a temperature of 20 ± 0,01 °C; or

Electronic assemblies specially designed to provide feedback capability in systems specified above;

2. Angular displacement measuring instruments;

(c) Equipment for measuring surface roughness (including surface defects), by measuring optical scatter with a sensitivity of 0,5 nm or less (better).

(a) Technical note:

Capable in real time of full three-dimensional image processing or full three-dimensional scene analysis to generate or modify programs or to generate or modify numerical program data; The scene analysis limitation does not include approximation of the third dimension by viewing at a given angle, or limited greyscale interpretation for the perception of depth or texture for the approved tasks (2 1/2 D).

(b) Specially designed to comply with national safety standards applicable to potentially explosive munitions environments;

(c) Specially designed or rated as radiation-hardened to withstand greater than 5 × 103 Gy (Si) without operational degradation; or

(d) Specially designed to operate at altitudes exceeding 30000 m.

(a) Linear position feedback units having an overall accuracy less (better) than (800 + (600 × L/1000)) nm (L equals the effective length in mm);

(b) Rotary position feedback units having an accuracy less (better) than 0,00025 °; or

(c) Compound rotary tables and tilting spindles, for use with machine tools to or above the levels specified by this category.

(a) Three or more axes which can be coordinated simultaneously for contouring control; and

(b) A roller force more than 60 kN.

IX.A3.4. Notes: 1.2. Notes: 1.2. Technical notes: 1.2. Technical note: Technical notes: 1.2.3.4.5.6.7. Technical notes: 1.2.3.4. Notes: 1.2. Technical notes: 1.2.

ELECTRONICS No Description Related item from Annex I to Regulation (EC) No 428/2009 IX.A3.001 Electronic items, as follows: 3A001.a IX.A3.002 Integrated circuits designed or rated as radiation hardened to withstand any of the following: Note: The category above does not apply to Metal Insulator Semiconductors (MIS). 3A001.a. IX.A3.003 Microprocessor microcircuits, microcomputer microcircuits, microcontroller microcircuits, storage integrated circuits manufactured from a compound semiconductor, analogue-to-digital converters, integrated circuits that contain analogue-to-digital converters and store or process the digitized data, digital-to-analogue converters, electro-optical or optical integrated circuits designed for signal processing, field programmable logic devices, custom integrated circuits for which either the function is unknown or the status of the equipment in which the integrated circuit will be used is unknown, Fast Fourier Transform (FFT) processors, Electrical Erasable Programmable Read-Only Memories (EEPROMs), flash memories, Static Random-Access Memories (SRAMs) or Magnetic Random-Access Memories (MRAMs), having any of the following: Note: This category does not apply to integrated circuits for civil automobile or railway train applications. 3A001.a.2 IX.A3.004 Electro-optical and optical integrated circuits, designed for signal processing and having all of the following: 3A001.a. IX.A3.005 Field programmable logic devices having any of the following: Note: This category includes 3A001.a. IX.A3.006 Neural network integrated circuits; 3A001.a. IX.A3.007 Custom integrated circuits for which the function is unknown, or the status of the equipment in which the integrated circuits will be used is unknown to the manufacturer, having any of the following: 3A001.a. IX.A3.008 Direct Digital Synthesizer (DDS) integrated circuits having any of the following: Technical note: The DAC clock frequency may be specified as the master clock frequency or the input clock frequency. 3A001.a. IX.A3.009 Microwave or millimetre wave items, as follows: Technical note: Dual mode means that the vacuum electronic device beam current can be intentionally changed between continuous-wave and pulsed mode operation by use of a grid and produces a peak pulse output power greater than the continuous-wave output power. 3A001.b. IX.A3.010 Monolithic Microwave Integrated Circuit (MMIC) amplifiers that are any of the following: The status of the MMIC whose rated operating frequency includes frequencies listed in more than one frequency range is determined by the lowest peak saturated power output threshold. This category does not apply to MMICs if they are specially designed for other applications, e.g., telecommunications, radar, automobiles. 3A001.b. IX.A3.011 Discrete microwave transistors that are any of the following: The status of a transistor whose rated operating frequency includes frequencies listed in more than one frequency range is determined by the lowest peak saturated power output threshold. This category includes bare dice, dice mounted on carriers or dice mounted in packages. Some discrete transistors may also be referred to as power amplifiers. 3A001.b. IX.A3.012 Microwave solid-state amplifiers and microwave assemblies/modules containing microwave solid-state amplifiers that are any of the following: Note: The status of an item whose rated operating frequency includes frequencies listed in more than one frequency range is determined by the lowest peak saturated power output threshold. 3A001.b. IX.A3.013 Electronically or magnetically tunable band-pass or band-stop filters, having more than 5 tunable resonators capable of tuning across a 1,5:1 frequency band (fmax/fmin) in less than 10 μs and having any of the following: 3A001.b. IX.A3.014 Converters and harmonic mixers that are any of the following: 3A001.b. IX.A3.015 Microwave power amplifiers containing vacuum electronic devices specified above and having all of the following: Note: This category does not apply to equipment designed or rated for operation in any frequency band which is allocated by the International Telecommunication Union (ITU) for radio communications services, but not for radio determination. 3A001.b. IX.A3.016 Microwave Power Modules (MPMs) consisting of, at least, a travelling-wave vacuum electronic device, a Monolithic Microwave Integrated Circuit (MMIC) and an integrated electronic power conditioner and having all of the following: To calculate the volume in item b. above, the following example is provided: for a maximum rated power of 20 W, the volume would be: 20 W × 10 cm3/W = 200 cm3. The turn-on time in item a. above refers to the time from fully off to fully operational, i.e., it includes the warm-up time of the MPM. 3A001.b. IX.A3.017 Oscillators or oscillator assemblies, specified to operate with a single sideband (SSB) phase noise, in dBc/Hz, less (better) than -(126 + 20log10F -20log10f) anywhere within the range of 10 Hz ≤ F ≤ 10 kHz; In the category above, F is the offset from the operating frequency in Hz and f is the operating frequency in MHz. 3A001.b. IX.A3.018 Frequency synthesizer electronic assemblies having a frequency switching time as specified by any of the following: 3A001.b. IX.A3.019 Transmit/receive modules, transmit/receive MMICs, transmit modules and transmit MMICs, rated for operation at frequencies above 2,7 GHz and having all of the following: A transmit/receive module is a multifunction electronic assembly that provides bidirectional amplitude and phase control for transmission and reception of signals. A transmit module is an electronic assembly that provides amplitude and phase control for transmission of signals. A transmit/receive MMIC is a multifunction MMIC that provides bidirectional amplitude and phase control for transmission and reception of signals. A transmit MMIC is a MMIC that provides amplitude and phase control for transmission of signals. 2,7 GHz should be used as the lowest operating frequency (fGHz) in the formula in item (c) for transmit/receive or transmit modules that have a rated operation range extending downward to 2,7 GHz and below [d ≤15 cm * GHz * N/2,7 GHz]. Item IX.A3.019 applies to transmit/receive modules or transmit modules with or without a heat sink. The value of d in item 11.c. does not include any portion of the transmit/receive module or transmit module that functions as a heat sink. Transmit/receive modules, transmit modules, transmit/receive MMICs or transmit MMICs may or may not have N integrated radiating antenna elements where N is the number of transmit or transmit/receive channels. 3A001.b. IX.A3.020 Surface acoustic wave and surface skimming (shallow bulk) acoustic devices with any of the following: 3A001.c. IX.A3.021 Bulk (volume) acoustic wave which permit the direct processing of signals at frequencies exceeding 6 GHz; 3A001.c. IX.A3.022 Acoustic-optic signal processing devices employing interaction between acoustic waves (bulk wave or surface wave) and light waves which permit the direct processing of signals or images, including spectral analysis, correlation or convolution; 3A001.c. IX.A3.023 Electronic devices and circuits containing components, manufactured from superconductive materials, specially designed for operation at temperatures below the critical temperature of at least one of the superconductive constituents and having any of the following: 3A001.d. IX.A3.024 High-energy cells, as follows: For the purposes of high-energy devices, energy density (Wh/kg) is calculated from the nominal voltage multiplied by the nominal capacity in ampere-hours (Ah) divided by the mass in kilograms. If the nominal capacity is not stated, energy density is calculated from the nominal voltage squared, then multiplied by the discharge duration in hours divided by the discharge load in Ohms and the mass in kilograms. For the purposes of high-energy devices, a cell is defined as an electrochemical device, which has positive and negative electrodes and an electrolyte, and is a source of electrical energy. It is the basic building block of a battery. For the purposes of high-energy devices, a primary cell is a cell that is not designed to be charged by any other source. For the purposes of high-energy devices, a secondary cell is a cell that is designed to be charged by an external electrical source. Note: High-energy devices do not apply to batteries, including single-cell batteries. 3A001.e. IX.A3.025 High-energy storage capacitors, as follows: 3A001.e. IX.A3.026 Superconductive electromagnets and solenoids, specially designed to be fully charged or discharged in less than one second and having all of the following: Note: The item above does not apply to superconductive electromagnets or solenoids specially designed for Magnetic Resonance Imaging (MRI) medical equipment. 3A001.e. IX.A3.027 Solar cells, cell-interconnect-coverglass (CIC) assemblies, solar panels, and solar arrays, which are space-qualified, having a minimum average efficiency exceeding 20 % at an operating temperature of 301 K (28 °C) under simulated AM0 illumination with an irradiance of 1367 watts per square metre (W/m2); Technical note: AM0, or Air Mass Zero, refers to the spectral irradiance of sunlight in the Earth's outer atmosphere when the distance between the Earth and the sun is one astronomical unit (AU). 3A001.e. IX.A3.028 Rotary input type absolute position encoders having an accuracy equal to or less (better) than 1,0 second of arc and specially designed encoder rings, discs or scales therefor; 3A001.f. IX.A3.029 Solid-state pulsed power switching thyristor devices and thyristor modules, using either electrically, optically or electron radiation controlled switch methods and having any of the following: Item (g) above includes: Item (g) above does not apply to thyristor devices and thyristor modules incorporated into equipment designed for civil railway or civil aircraft applications. Technical note: For the purposes of item (g) above, a thyristor module contains one or more thyristor devices. 3A001.g. IX.A3.030 Solid-state power semiconductor switches, diodes or modules, having all of the following: Note: Repetitive peak off-state voltage in the item above includes drain to source voltage, collector to emitter voltage, repetitive peak reverse voltage and peak repetitive off-state blocking voltage. 3A001.h. IX.A3.031 Recording equipment and oscilloscopes, as follows 3A002.a. IX.A3.032 Signal analysers, as follows: Probability of discovery in item 1. above is also referred to as probability of intercept or probability of capture. For the purposes of item 1. above, the duration for 100 % probability of discovery is equivalent to the minimum signal duration necessary for the specified level measurement uncertainty. Note: The category above does not apply to those signal analysers using only constant percentage bandwidth filters (also known as octave or fractional octave filters). 3A002.c. IX.A3.033 Signal generators having any of the following: 3A002.d. IX.A3.034 Network analysers having any of the following: Technical note: Non-linear vector measurement functionality is an instrument's ability to analyse the test results of devices driven into the large-signal domain or the non-linear distortion range. 3A002.e. IX.A3.035 Microwave test receivers having all of the following; 3A002.f. IX.A3.036 Atomic frequency standards being any of the following: 3A002.f. IX.A3.037 Equipment for the manufacturing of semiconductor devices or materials, as follows and specially designed components and accessories therefor: 3B001.b. 3B001.f. 3B001.f. IX.A3.038 Equipment designed for device processing using direct writing methods; Masks and reticles, designed for integrated circuits. 3B001.g. IX.A3.038 Test equipment specially designed for testing finished or unfinished semiconductor and microwave devices as follows and specially designed components and accessories therefor: 3B002 IX.A3.039 Hetero-epitaxial materials consisting of a substrate having stacked epitaxially grown multiple layers with any of the following: Note: This item does not apply to a substrate having one or more P-type epitaxial layers of GaN, InGaN, AlGaN, InAlN, InAlGaN, GaP, GaAs, AlGaAs, InP, InGaP, AlInP or InGaAlP, independent of the sequence of the elements, except if the P-type epitaxial layer is between N-type layers. 3C001 IX.A3.040 Resist materials as follows and substrates coated with the following resists: 3C002 IX.A3.041 Organo-inorganic compounds: 3C003 IX.A3.042 Hydrides of phosphorus, arsenic or antimony, having a purity better than 99,999 %, even diluted in inert gases or hydrogen. Note: The item above does not apply to hydrides containing 20 % molar or more of inert gases or hydrogen. 3C004 IX.A3.043 Silicon carbide (SiC), gallium nitride (GaN), aluminium nitride (AlN) or aluminium gallium nitride (AlGaN) semiconductor substrates, or ingots, boules or other preforms of those materials, having resistivities greater than 10000 ohm-cm at 20 °C. 3C005 IX.A3.044 Substrates specified in item 5 above with at least one epitaxial layer of silicon carbide, gallium nitride, aluminium nitride or aluminium gallium nitride. 3C006

IX.A3. (a) Notes: 1.2.

General-purpose integrated circuits, as follows: The status of wafers (finished or unfinished), in which the function has been determined, is to be evaluated against the parameters of 3A001.a. 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;

Monolithic Microwave Integrated Circuits (MMICs).

(a) A total dose of 5 × 103 Gy (Si) or higher;

(b) A dose rate upset of 5 × 106 Gy (Si)/s or higher; or

(c) A fluence (integrated flux) of neutrons (1 MeV equivalent) of 5 × 1013 n/cm2 or higher on silicon, or its equivalent for other materials;

(a) Rated for operation at an ambient temperature above 398 K (+ 125 °C);

(b) Rated for operation at an ambient temperature below 218 K (– 55 °C); or

(a) One or more than one internal laser diode;

(b) One or more than one internal light detecting element; and

IX.A3.4.

(a) A maximum number of single-ended digital input/outputs of greater than 700; or

(b) An aggregate one-way peak serial transceiver data rate of 500 Gb/s or greater;

Simple Programmable Logic Devices (SPLDs);

Complex Programmable Logic Devices (CPLDs);

Field Programmable Gate Arrays (FPGAs);

Field Programmable Logic Arrays (FPLAs);

Field Programmable Interconnects (FPICs).

(a) More than 1500 terminals;

(b) A typical basic gate propagation delay time of less than 0,02 ns; or

(a) A Digital-to-Analogue Converter (DAC) clock frequency of 3,5 GHz or more and a DAC resolution of 10 bit or more, but less than 12 bit; or

(b) A DAC clock frequency of 1,25 GHz or more and a DAC resolution of 12 bit or more;

(a) Travelling-wave vacuum electronic devices, pulsed or continuous wave;

(a)

1. Devices operating at frequencies exceeding 31,8 GHz;

2. Devices having a cathode heater with a turn-on time to rated RF power of less than 3 seconds;

3. Coupled cavity devices, or derivatives thereof, with a fractional bandwidth of more than 7 % or a peak power exceeding 2,5 kW;

4. Devices based on helix, folded waveguide, or serpentine waveguide circuits, or derivatives thereof, having any of the following:

4. a.

An instantaneous bandwidth of more than one octave, and average power (expressed in kW) times frequency (expressed in GHz) of more than 0,5;

An instantaneous bandwidth of one octave or less, and average power (expressed in kW) times frequency (expressed in GHz) of more than 1;

Being space-qualified; or

Having a gridded electron gun;

5. Devices with a fractional bandwidth of greater than or equal to 10 %, with any of the following:

5. a.

An annular electron beam;

A non-axisymmetric electron beam; or

Multiple electron beams;

(b) Crossed-field amplifier vacuum electronic devices with a gain of more than 17 dB;

(c) Thermionic cathodes designed for vacuum electronic devices producing an emission current density at rated operating conditions exceeding 5 A/cm2 or a pulsed (non-continuous) current density at rated operating conditions exceeding 10 A/cm2;

(d) Vacuum electronic devices with the capability to operate in a dual mode;

(a) Rated for operation at frequencies exceeding 2,7 GHz up to and including 6,8 GHz with a fractional bandwidth of greater than 15 %, and having any of the following:

(a)

1. A peak saturated power output greater than 75 W (48,75 dBm) at any frequency exceeding 2,7 GHz up to and including 2,9 GHz;

2. A peak saturated power output greater than 55 W (47,4 dBm) at any frequency exceeding 2,9 GHz up to and including 3,2 GHz;

3. A peak saturated power output greater than 40 W (46 dBm) at any frequency exceeding 3,2 GHz up to and including 3,7 GHz; or

4. A peak saturated power output greater than 20 W (43 dBm) at any frequency exceeding 3,7 GHz up to and including 6,8 GHz;

(b) Rated for operation at frequencies exceeding 6,8 GHz up to and including 16 GHz with a fractional bandwidth of greater than 10 %, and having any of the following:

(b)

1. A peak saturated power output greater than 10W (40 dBm) at any frequency exceeding 6,8 GHz up to and including 8,5 GHz; or

2. A peak saturated power output greater than 5W (37 dBm) at any frequency exceeding 8,5 GHz up to and including 16 GHz;

(c) Rated for operation with a peak saturated power output greater than 3 W (34,77 dBm) at any frequency exceeding 16 GHz up to and including 31,8 GHz, and with a fractional bandwidth of greater than 10 %;

(d) Rated for operation with a peak saturated power output greater than 0,1n W (– 70 dBm) at any frequency exceeding 31,8 GHz up to and including 37 GHz;

(e) Rated for operation with a peak saturated power output greater than 1 W (30 dBm) at any frequency exceeding 37 GHz up to and including 43,5 GHz, and with a fractional bandwidth of greater than 10 %;

(f) Rated for operation with a peak saturated power output greater than 31,62 mW (15 dBm) at any frequency exceeding 43,5 GHz up to and including 75 GHz, and with a fractional bandwidth of greater than 10 %;

(g) Rated for operation with a peak saturated power output greater than 10 mW (10 dBm) at any frequency exceeding 75 GHz up to and including 90 GHz, and with a fractional bandwidth of greater than 5 %; or

(h) Rated for operation with a peak saturated power output greater than 0,1 nW (– 70 dBm) at any frequency exceeding 90 GHz;

IX.A3.4. Notes: 1.2. a.

Rated for operation at frequencies exceeding 2,7 GHz up to and including 6,8 GHz and having any of the following:

1. A peak saturated power output greater than 400 W (56 dBm) at any frequency exceeding 2,7 GHz up to and including 2,9 GHz;

2. A peak saturated power output greater than 205 W (53,12 dBm) at any frequency exceeding 2,9 GHz up to and including 3,2 GHz;

3. A peak saturated power output greater than 115 W (50,61 dBm) at any frequency exceeding 3,2 GHz up to and including 3,7 GHz; or

4. A peak saturated power output greater than 60 W (47,78 dBm) at any frequency exceeding 3,7 GHz up to and including 6,8 GHz;

Rated for operation at frequencies exceeding 6,8 GHz up to and including 31,8 GHz and having any of the following:

1. A peak saturated power output greater than 50 W (47 dBm) at any frequency exceeding 6,8 GHz up to and including 8,5 GHz;

2. A peak saturated power output greater than 15 W (41,76 dBm) at any frequency exceeding 8,5 GHz up to and including 12 GHz;

3. A peak saturated power output greater than 40 W (46 dBm) at any frequency exceeding 12 GHz up to and including 16 GHz; or

4. A peak saturated power output greater than 7 W (38,45 dBm) at any frequency exceeding 16 GHz up to and including 31,8 GHz;

Rated for operation with a peak saturated power output greater than 0,5 W (27 dBm) at any frequency exceeding 31,8 GHz up to and including 37 GHz;

Rated for operation with a peak saturated power output greater than 1 W (30 dBm) at any frequency exceeding 37 GHz up to and including 43,5 GHz; or

Rated for operation with a peak saturated power output greater than 0,1 nW (-70 dBm) at any frequency exceeding 43,5 GHz;

IX.A3.4. Notes: 1.2. Notes: 1.2.

(a) Rated for operation at frequencies exceeding 2,7 GHz up to and including 6,8 GHz with a fractional bandwidth of greater than 15 % and having any of the following:

(a)

1. A peak saturated power output greater than 500 W (57 dBm) at any frequency exceeding 2,7 GHz up to and including 2,9 GHz;

2. A peak saturated power output greater than 270 W (54,3 dBm) at any frequency exceeding 2,9 GHz up to and including 3,2 GHz;

3. A peak saturated power output greater than 200 W (53 dBm) at any frequency exceeding 3,2 GHz up to and including 3,7 GHz; or

4. A peak saturated power output greater than 90 W (49,54 dBm) at any frequency exceeding 3,7 GHz up to and including 6,8 GHz;

(b) Rated for operation at frequencies greater than 6,8 GHz up to and including 31,8 GHz with a fractional bandwidth of greater than 10 % and having any of the following:

(b)

1. A peak saturated power output greater than 70 W (48,54 dBm) at any frequency exceeding 6,8 GHz up to and including 8,5 GHz;

2. A peak saturated power output greater than 50 W (47 dBm) at any frequency exceeding 8,5 GHz up to and including 12 GHz;

3. A peak saturated power output greater than 30 W (44,77 dBm) at any frequency exceeding 12 GHz up to and including 16 GHz; or

4. A peak saturated power output greater than 20 W (43 dBm) at any frequency exceeding 16 GHz up to and including 31,8 GHz;

(c) Rated for operation with a peak saturated power output greater than 0,5 W (27 dBm) at any frequency exceeding 31,8 GHz up to and including 37 GHz;

(d) Rated for operation with a peak saturated power output greater than 2 W (33 dBm) at any frequency exceeding 37 GHz up to and including 43,5 GHz, and with a fractional bandwidth of greater than 10 %;

(e) Rated for operation at frequencies exceeding 43,5 GHz and having any of the following:

(e)

1. A peak saturated power output greater than 0,2 W (23 dBm) at any frequency exceeding 43,5 GHz up to and including 75 GHz, and with a fractional bandwidth of greater than 10 %;

2. A peak saturated power output greater than 20 mW (13 dBm) at any frequency exceeding 75 GHz up to and including 90 GHz, and with a fractional bandwidth of greater than 5 %; or

3. A peak saturated power output greater than 0,1 nW (- 70 dBm) at any frequency exceeding 90 GHz;

(a) A band-pass bandwidth of more than 0,5 % of centre frequency; or

(b) A band-stop bandwidth of less than 0,5 % of centre frequency;

(a) Designed to extend the frequency range of signal analysers beyond 90 GHz;

(b) Designed to extend the operating range of signal generators as follows:

(b)

1. Beyond 90 GHz;

2. To an output power greater than 100 mW (20 dBm) anywhere within the frequency range exceeding 43,5 GHz but not exceeding 90 GHz;

(c)

1. Beyond 110 GHz;

2. To an output power greater than 31,62 mW (15 dBm) anywhere within the frequency range exceeding 43,5 GHz but not exceeding 90 GHz;

3. To an output power greater than 1 mW (0 dBm) anywhere within the frequency range exceeding 90 GHz but not exceeding 110 GHz; or

(d) Designed to extend the frequency range of microwave test receivers beyond 110 GHz;

(a) Operating frequencies above 3 GHz;

(b) An average output power to mass ratio exceeding 80 W/kg; and

(a) A turn-on time from off to fully operational in less than 10 seconds;

(b) A volume less than the maximum rated power in watts multiplied by 10 cm3/W; and

(c)

1. For frequencies equal to or less than 18 GHz, an RF output power greater than 100 W; or

2. A frequency greater than 18 GHz;

IX.A3.4. Notes: 1.2. Notes: 1.2. Technical notes: 1.2. Technical note:

(a) Less than 143 ps;

(b) Less than 100 μs for any frequency change exceeding 2,2 GHz within the synthesized frequency range exceeding 4,8 GHz but not exceeding 31,8 GHz;

(c) Less than 500 μs for any frequency change exceeding 550 MHz within the synthesized frequency range exceeding 31,8 GHz but not exceeding 37 GHz;

(d) Less than 100 μs for any frequency change exceeding 2,2 GHz within the synthesized frequency range exceeding 37 GHz but not exceeding 90 GHz; or

(e) Less than 1 ms within the synthesized frequency range exceeding 90 GHz;

(a) A peak saturated power output (in watts), Psat, greater than 505,62 divided by the maximum operating frequency (in GHz) squared [Psat > 505,62 W * GHz2/fGHz2] for any channel;

(b) A fractional bandwidth of 5 % or greater for any channel;

(c) Any planar side with length d (in cm) equal to or less than 15 divided by the lowest operating frequency in GHz [d ≤ 15 cm * GHz * N/fGHz] where N is the number of transmit or transmit/receive channels; and

An electronically variable phase shifter per channel;

IX.A3.4. Notes: 1.2. Notes: 1.2. Technical notes: 1.2. Technical note: Technical notes: 1.2.3.4.5.6.7.

(a) A carrier frequency exceeding 6 GHz;

(b) A carrier frequency exceeding 1 GHz, but not exceeding 6 GHz and having any of the following:

(b)

1. A frequency side-lobe rejection exceeding 65 dB;

2. A product of the maximum delay time and the bandwidth (time in μs and bandwidth in MHz) of more than 100;

3. A bandwidth of greater than 250 MHz; or

4. A dispersive delay of more than 10 μs; or

(c)

1. A product of the maximum delay time and the bandwidth (time in μs and bandwidth in MHz) of more than 100;

2. A dispersive delay of more than 10 μs; or

3. A frequency side-lobe rejection exceeding 65 dB and a bandwidth greater than 100 MHz;

(a) Current switching for digital circuits using superconductive gates with a product of delay time per gate (in seconds) and power dissipation per gate (in watts) of less than 10– 14 J; or

(b) Frequency selection at all frequencies using resonant circuits with Q-values exceeding 10000;

(a) Primary cells having an energy density exceeding 550 Wh/kg at 20 °C;

(b) Secondary cells having an energy density exceeding 350 Wh/kg at 20 °C;

IX.A3.4. Notes: 1.2. Notes: 1.2. Technical notes: 1.2. Technical note: Technical notes: 1.2.3.4.5.6.7. Technical notes: 1.2.3.4.

(a) Capacitors with a repetition rate of less than 10 Hz (single shot capacitors) and having all of the following:

(a)

1. A voltage rating equal to or more than 5 kV;

2. An energy density equal to or more than 250 J/kg; and

3. A total energy equal to or more than 25 kJ;

(b) Capacitors with a repetition rate of 10 Hz or more (repetition rated capacitors) and having all of the following:

(b)

1. A voltage rating equal to or more than 5 kV;

2. An energy density equal to or more than 50 J/kg;

3. A total energy equal to or more than 100 J; and

4. A charge/discharge cycle life equal to or more than 10000;

(a) Energy delivered during the discharge exceeding 10 kJ in the first second;

(b) Inner diameter of the current carrying windings of more than 250 mm; and

1. A maximum turn-on current rate of rise (di/dt) greater than 30000 A/μs and off-state voltage greater than 1100 V; or

2. A maximum turn-on current rate of rise (di/dt) greater than 2000 A/μs and having all of the following:

2. a.

An off-state peak voltage equal to or greater than 3000 V; and

A peak (surge) current equal to or greater than 3000 A;

Silicon Controlled Rectifiers (SCRs);

Electrical Triggering Thyristors (ETTs);

Light Triggering Thyristors (LTTs);

Integrated Gate Commutated Thyristors (IGCTs);

Gate Turn-off Thyristors (GTOs);

MOS Controlled Thyristors (MCTs);

Solidtrons.

IX.A3.4. Notes: 1.2. Notes: 1.2. Technical notes: 1.2. Technical note: Technical notes: 1.2.3.4.5.6.7. Technical notes: 1.2.3.4. Notes: 1.2.

1. Rated for a maximum operating junction temperature greater than 488 K (215 °C);

2. Repetitive peak off-state voltage (blocking voltage) exceeding 300 V; and

3. Continuous current greater than 1 A.

1. Technical notes: 1.2.

Digital data recorders having all of the following: For recorders with a parallel bus architecture, the continuous throughput rate is the highest word rate multiplied by the number of bits in a word. Continuous throughput is the fastest data rate the instrument can record to disk or solid-state drive memory without the loss of any information while sustaining the input digital data rate or digitizer conversion rate.

1. a.

A sustained continuous throughput of more than 6,4 Gbit/s to disk or solid-state drive memory; and

A processor that performs analysis of radio frequency signal data while it is being recorded;

2. Real-time oscilloscopes having a vertical root-mean-square (rms) noise voltage of less than 2 % of full-scale at the vertical scale setting that provides the lowest noise value for any input 3 dB bandwidth of 60 GHz or greater per channel;

1. Signal analysers having a 3 dB resolution bandwidth (RBW) exceeding 10 MHz anywhere within the frequency range exceeding 31,8 GHz but not exceeding 37 GHz;

2. Signal analysers having Displayed Average Noise Level (DANL) less (better) than - 150 dBm/Hz anywhere within the frequency range exceeding 43,5 GHz but not exceeding 90 GHz;

3. Signal analysers having a frequency exceeding 90 GHz;

4. Signal analysers having all of the following:

4. a.

Real-time bandwidth exceeding 170 MHz; and

Having any of the following:

1. 100 % probability of discovery, with less than a 3 dB reduction from full amplitude due to gaps or windowing effects, of signals having a duration of 15 μs or less; or

2. A frequency mask trigger function with 100 % probability of trigger (capture) for signals having a duration of 15 μs or less;

IX.A3.4. Notes: 1.2. Notes: 1.2. Technical notes: 1.2. Technical note: Technical notes: 1.2.3.4.5.6.7. Technical notes: 1.2.3.4. Notes: 1.2. Technical notes: 1.2.

1. Specified to generate pulse-modulated signals having all of the following, anywhere within the frequency range exceeding 31,8 GHz but not exceeding 37 GHz:

1. a.

Pulse duration of less than 25 ns; and

On/off ratio equal to or exceeding 65 dB;

2. An output power exceeding 100 mW (20 dBm) anywhere within the frequency range exceeding 43,5 GHz but not exceeding 90 GHz;

3. A frequency switching time as specified by any of the following:

3. a.

Less than 100 μs for any frequency change exceeding 2,2 GHz within the frequency range exceeding 4,8 GHz but not exceeding 31,8 GHz

Less than 500 μs for any frequency change exceeding 550 MHz within the frequency range exceeding 31,8 GHz but not exceeding 37 GHz; or

Less than 100 μs for any frequency change exceeding 2,2 GHz within the frequency range exceeding 37 GHz but not exceeding 90 GHz;

1. An output power exceeding 31,62 mW (15 dBm) anywhere within the operating frequency range exceeding 43,5 GHz but not exceeding 90 GHz;

2. An output power exceeding 1 mW (0 dBm) anywhere within the operating frequency range exceeding 90 GHz but not exceeding 110 GHz;

3. Non-linear vector measurement functionality at frequencies exceeding 50 GHz but not exceeding 110 GHz; or

4. A maximum operating frequency exceeding 110 GHz;

1. A maximum operating frequency exceeding 110 GHz; and

2. Being capable of measuring amplitude and phase simultaneously;

1. Space-qualified;

2. Non-rubidium and having a long-term stability less (better) than 1 × 10– 11/month; or

3. Non-space-qualified and having all of the following:

3. a.

Being a rubidium standard;

Long-term stability less (better) than 1 × 10– 11/month; and

Total power consumption of less than 1 Watt.

(a) Equipment designed for ion implantation and having any of the following:

(a)

1. Being designed and optimized to operate at a beam energy of 20 keV or more and a beam current of 10 mA or more for hydrogen, deuterium or helium implant;

2. Direct write capability;

3. A beam energy of 65 keV or more and a beam current of 45 mA or more for high-energy oxygen implant into a heated semiconductor material substrate; or

4. Being designed and optimized to operate at a beam energy of 20 keV or more and a beam current of 10 mA or more for silicon implant into a semiconductor material substrate heated to 600 °C or greater;

(b) Lithography equipment as follows and imprint lithography equipment capable of producing features of 45 nm or less: Technical note: The Minimum Resolvable Feature size (MRF) is calculated by the following formula: MRFan exposure light source wavelength in nmK factornumerical aperture where the K factor = 0,35

(b)

1. Align and expose step and repeat (direct step on wafer) or step and scan (scanner) equipment for wafer processing using photo-optical or X-ray methods and having any of the following:

1. a.

A light source wavelength shorter than 193 nm; or

Capable of producing a pattern with a Minimum Resolvable Feature size (MRF) of 45 nm or less;

(a) For testing S-parameters of transistor devices at frequencies exceeding 31,8 GHz;

(b) For testing microwave integrated circuits specified above.

(a) Silicon (Si);

(b) Germanium (Ge);

(d) III/V compounds of gallium or indium.

(a) Resists designed for semiconductor lithography as follows:

(a)

1. Positive resists adjusted (optimized) for use at wavelengths less than 245 nm but equal to or greater than 15 nm;

2. Resists adjusted (optimized) for use at wavelengths less than 15 nm but greater than 1 nm;

(b) All resists designed for use with electron beams or ion beams, with a sensitivity of 0,01 μcoulomb/mm2 or better;

(d) All resists designed or optimized for use with imprint lithography equipment capable of producing features of 45 nm or less that use either a thermal or photo-curable process.

(a) Organo-metallic compounds of aluminium, gallium or indium, having a purity (metal basis) better than 99,999 %;

(b) Organo-arsenic, organo-antimony and organo-phosphorus compounds, having a purity (inorganic element basis) better than 99,999 %.

IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2. Technical note: Notes: 1.2. Technical note: 1. Technical note: Technical notes: 1.2.

SENSORS AND LASERS No Description Related item from Annex I to Regulation (EC) No 428/2009 IX.A6.001 Optical sensors or equipment and components therefor, as follows: 6A002.d. IX.A6.002 Non-space-qualified cryocoolers having a cooling source temperature below 218 K (– 55 °C), as follows: 6A002.d. IX.A6.003 Optical sensing fibres specially fabricated either compositionally or structurally, or modified by coating, to be acoustically, thermally, inertially, electromagnetically or nuclear radiation sensitive. 6A002.d. IX.A6.004 Cameras, systems or equipment, and components therefor, as follows: 6A003 IX.A6.005 High-speed cinema recording cameras using any film format from 8 mm to 16 mm inclusive, in which the film is continuously advanced throughout the recording period, and that are capable of recording at framing rates exceeding 13150 frames/s; Note: The item above does not apply to cinema recording cameras designed for civil purposes. 6A003 IX.A6.006 Imaging cameras, as follows: Note: The item above does not apply to television or video cameras, specially designed for television broadcasting. For the purposes of this entry, digital video cameras should be evaluated by the maximum number of active pixels used for capturing moving images. For the purposes of this entry, camera tracking data is the information necessary to define camera line of sight orientation with respect to the Earth. This includes: (a) the horizontal angle the camera line of sight makes with respect to the Earth's magnetic field direction; and (b) the vertical angle between the camera line of sight and the Earth's horizon. 6A003 IX.A6.007 Scanning cameras and scanning camera systems; Note: The item above does not apply to scanning cameras and scanning camera systems, specially designed for any of the following: 6A003 IX.A6.008 Imaging cameras incorporating image intensifier tubes having any of the following: 6A003 IX.A6.009 Imaging cameras incorporating focal plane arrays having any of the following: Imaging cameras specified in item 4 above include focal plane arrays combined with sufficient signal processing electronics, beyond the read-out integrated circuit, to enable as a minimum the output of an analogue or digital signal once power is supplied. Item 4.a. does not apply to imaging cameras incorporating linear focal plane arrays with 12 elements or fewer, not employing time-delay-and-integration within the element and designed for any of the following: Item 4.b. does not apply to imaging cameras having any of the following: 6A003 IX.A6.010 Optical mirrors (reflectors), as follows: Note: Items 2 and 3 above do not apply to mirrors specially designed to direct solar radiation for terrestrial heliostat installations. 6A004.a. IX.A6.011 Mirrors specially designed for beam steering mirror stages with a flatness of λ/10 or better (λ is equal to 633 nm) and having any of the following: 6A004.b. IX.A6.012 Optical components made from zinc selenide (ZnSe) or zinc sulphide (ZnS) with transmission in the wavelength range exceeding 3000 nm but not exceeding 25000 nm and having any of the following: 6A004.c. IX.A6.013 Non-tunable continuous-wave (CW) lasers having any of the following: Item b. above does not apply to 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 purposes 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. Item b. above does not apply to multiple transverse mode, industrial lasers having any of the following: For the purposes of 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. 6A005.a.1. 6A005.a.2.. 6A005.a.3 6A005.a.4. 6A005.a.5. 6A005.a.6. IX.A6.014 Tunable lasers having any of the following: 6A005.c. IX.A6.015 Other semiconductor lasers, as follows: Includes semiconductor lasers having optical output connectors (e.g., fibre-optic pigtails). The status of semiconductor lasers specially designed for other equipment is determined by the status of the other equipment. For the purposes of this category power density means the total laser output power divided by the emitter surface area of the stacked array. 6A005.d.1 IX.A6.016 Chemical lasers, as follows: 6A005.d.5 IX.A6.017 Components, as follows: 6A005.e. IX.A6.018 Gravity meters (gravimeters) and gravity gradiometers, as follows: 6A007 IX.A6.019 Radar systems, equipment and assemblies, having any of the following, and specially designed components therefor: Note: This section does not apply to: 6A008 IX.A6.020 Optical equipment, as follows: Note: The item above does not apply to microscopes. 6B004 IX.A6.021 Equipment to produce, align and calibrate land-based gravity meters with a static accuracy of better than 0,1 mGal. 6B007 IX.A6.022 Pulse radar cross-section measurement systems having transmit pulse widths of 100 ns or less, and specially designed components therefor. 6B008 IX.A6.023 Optical sensor materials, as follows: Mole fraction is defined as the ratio of moles of ZnTe to the sum of the moles of CdTe and ZnTe present in the crystal. 6C002 IX.A6.024 Optical materials, as follows: 6C004.a. 6C004.b. IX.A6.025 Substrate blanks of silicon carbide or beryllium beryllium (Be/Be) deposited materials, exceeding 300 mm in diameter or major axis length; 6C004.d. IX.A6.026 Glass, including fused silica, phosphate glass, fluorophosphate glass, zirconium fluoride (ZrF4) (CAS 7783-64-4) and hafnium fluoride (HfF4) (CAS 13709-52-9) and having all of the following: 6C004.e. IX.A6.027 Laser materials, as follows: For the purposes of the item above, the core Numerical Aperture (NA) is measured at the emission wavelengths of the fibre. Item (b) above includes fibres assembled with end caps. 6C005

IX.A6.

(a) Special support components for optical sensors, as follows:

(a)

1. Space-qualified cryocoolers;

(a) Closed cycle type with a specified Mean-Time-To-Failure (MTTF) or Mean-Time-Between-Failures (MTBF), exceeding 2500 hours;

(b) Joule-Thomson (JT) self-regulating minicoolers having bore (outside) diameters of less than 8 mm;

(a) Instrumentation cameras and specially designed components therefor, as follows: Note: Instrumentation cameras, specified above, with modular structures should be evaluated by their maximum capability, using plug-ins available according to the camera manufacturer's specifications.

2. Mechanical high-speed cameras, in which the film does not move, capable of recording at rates exceeding 1000000 frames/s for the full framing height of 35 mm film, or at proportionately higher rates for lesser frame heights, or at proportionately lower rates for greater frame heights;

3. Mechanical or electronic streak cameras as follows:

3. a.

Mechanical streak cameras having writing speeds exceeding 10 mm/μs;

Electronic streak cameras having temporal resolution better than 50 ns;

4. Electronic framing cameras having a speed exceeding 1000000 frames/s;

5. Electronic cameras having all of the following:

5. a.

An electronic shutter speed (gating capability) of less than 1 μs per full frame; and

A read-out time allowing a framing rate of more than 125 full frames per second;

6. Plug-ins having all of the following characteristics:

6. a.

Specially designed for instrumentation cameras which have modular structures and which are specified in this item; and

Enabling these cameras to meet the characteristics specified above, according to the manufacturer's specifications;

1. Video cameras incorporating solid-state sensors, having a peak response in the wavelength range exceeding 10 nm, but not exceeding 30000 nm and having all of the following:

1. a.

Having any of the following:

1. More than 4 × 106 active pixels per solid-state array for monochrome (black and white) cameras;

2. More than 4 × 106 active pixels per solid-state array for colour cameras incorporating three solid-state arrays; or

3. More than 12 × 106 active pixels for solid-state array colour cameras incorporating one solid-state array; and

Having any of the following:

1. Optical mirrors specified below;

2. Optical control equipment specified below; or

3. The capability for annotating internally generated camera tracking data;

IX.A6. Technical notes: 1.2. a.

A peak response in the wavelength range exceeding 10 nm, but not exceeding 30000 nm;

Linear detector arrays with more than 8192 elements per array; and

Mechanical scanning in one direction;

(a) Industrial or civilian photocopiers;

(b) Image scanners specially designed for civil, stationary, close proximity scanning applications (e.g., reproduction of images or print contained in documents, artwork or photographs); or

Having all of the following:

1. A peak response in the wavelength range exceeding 400 nm but not exceeding 1050 nm;

2. Electron image amplification using any of the following:

2. a.

A microchannel plate with a hole pitch (centre-to-centre spacing) of 12 μm or less; or

An electron sensing device with a non-binned pixel pitch of 500 μm or less, specially designed or modified to achieve charge multiplication other than by a microchannel plate; and

3. Any of the following photocathodes:

3. a.

Multialkali photocathodes (e.g., S-20 and S-25) having a luminous sensitivity exceeding 350 μA/lm;

GaAs or GaInAs photocathodes; or

Other III/V compound semiconductor photocathodes having a maximum radiant sensitivity exceeding 10 mA/W; or

Having all of the following:

1. A peak response in the wavelength range exceeding 1050 nm but not exceeding 1800 nm;

2. Electron image amplification using any of the following:

2. a.

A microchannel plate with a hole pitch (centre-to-centre spacing) of 12 μm or less; or

An electron sensing device with a non-binned pixel pitch of 500 μm or less, specially designed or modified to achieve charge multiplication other than by a microchannel plate; and

3. III/V compound semiconductor (e.g., GaAs or GaInAs) photocathodes and transferred electron photocathodes, having a maximum radiant sensitivity exceeding 15 mA/W;

Incorporating non-space-qualified focal plane arrays having any of the following:

1. Having all of the following:

1. a.

Individual elements with a peak response within the wavelength range exceeding 900 nm but not exceeding 1050 nm; and

Any of the following:

1. A response time constant of less than 0,5 ns; or

2. Specially designed or modified to achieve charge multiplication and having a maximum radiant sensitivity exceeding 10 mA/W;

2. Having all of the following:

2. a.

Individual elements with a peak response in the wavelength range exceeding 1050 nm but not exceeding 1200 nm; and

Any of the following:

1. A response time constant of 95 ns or less; or

2. Specially designed or modified to achieve charge multiplication and having a maximum radiant sensitivity exceeding 10 mA/W; or

3. Being non-space-qualified non-linear (two-dimensional) focal plane arrays having individual elements with a peak response in the wavelength range exceeding 1200 nm but not exceeding 30000 nm;

4. Being non-space-qualified linear (one-dimensional) focal plane arrays having all of the following:

4. a.

Individual elements with a peak response in the wavelength range exceeding 1200 nm but not exceeding 3000 nm; and

Any of the following:

1. A ratio of scan direction dimension of the detector element to the cross-scan direction dimension of the detector element of less than 3,8; or

2. Signal processing in the detector elements; or

5. Being non-space-qualified linear (one-dimensional) focal plane arrays having individual elements with a peak response in the wavelength range exceeding 3000 nm but not exceeding 30000 nm;

Incorporating non-space-qualified non-linear (two-dimensional) infrared focal plane arrays based on microbolometer material having individual elements with an unfiltered response in the wavelength range equal to or exceeding 8000 nm but not exceeding 14000 nm; or

Incorporating non-space-qualified focal plane arrays having all of the following:

1. Individual detector elements with a peak response in the wavelength range exceeding 400 nm but not exceeding 900 nm;

2. Specially designed or modified to achieve charge multiplication and having a maximum radiant sensitivity exceeding 10 mA/W for wavelengths exceeding 760 nm; and

3. Greater than 32 elements.

IX.A6. Technical notes: 1.2. Notes: 1.2.

(a) Industrial or civilian intrusion alarm, traffic or industrial movement control or counting systems;

(b) Industrial equipment used for inspection or monitoring of heat flows in buildings, equipment or industrial processes;

(d) Equipment specially designed for laboratory use; or

(e) Medical equipment.

IX.A6. Technical notes: 1.2. Notes: 1.2.3.

(a) A maximum frame rate equal to or less than 9 Hz;

(b) Having all of the following:

(b)

1. Having a minimum horizontal or vertical Instantaneous Field of View (IFOV) of at least 10 mrad (milliradians);

2. Incorporating a fixed focal-length lens that is not designed to be removed;

3. Technical note:

Not incorporating a direct view display; and Direct view refers to an imaging camera operating in the infrared spectrum that presents a visual image to a human observer using a near-to-eye microdisplay incorporating any light-security mechanism.

4. Having any of the following:

4. a.

No facility to obtain a viewable image of the detected field of view; or

b. Technical note:

The camera is designed for a single kind of application and designed not to be user modified; or Instantaneous Field of View (IFOV) specified in note 3.b. is the lesser figure of the Horizontal IFOV or the Vertical IFOV. Horizontal IFOV = horizontal Field of View (FOV)/number of horizontal detector elements. Vertical IFOV = vertical Field of View (FOV)/number of vertical detector elements.

(c) The camera is specially designed for installation into a civilian passenger land vehicle and having all of the following:

(c)

1. The placement and configuration of the camera within the vehicle are solely to assist the driver in the safe operation of the vehicle.

1. Deformable mirrors having an active optical aperture greater than 10 mm and having any of the following, and specially designed components therefor:

1. a.

Having all the following:

1. A mechanical resonant frequency of 750 Hz or more; and

2. More than 200 actuators; or

A Laser Induced Damage Threshold (LIDT) being any of the following:

1. Greater than 1 kW/cm2 using a CW laser; or

2. Greater than 2 J/cm2 using 20 ns laser pulses at 20 Hz repetition rate;

2. Lightweight monolithic mirrors having an average equivalent density of less than 30 kg/m2 and a total mass exceeding 10 kg;

3. Lightweight composite or foam mirror structures having an average equivalent density of less than 30 kg/m2 and a total mass exceeding 2 kg;

Diameter or major axis length greater than or equal to 100 mm; or

Having all of the following:

1. Diameter or major axis length greater than 50 mm but less than 100 mm; and

2. A Laser Induced Damage Threshold (LIDT) being any of the following:

2. a.

Greater than 10 kW/cm2 using a CW laser; or

Greater than 20 J/cm2 using 20 ns laser pulses at 20 Hz repetition rate;

1. Exceeding 100 cm3 in volume; or

2. Exceeding 80 mm in diameter or length of major axis and 20 mm in thickness (depth);

(c)

1. Components lightweighted to less than 20 % equivalent density compared with a solid blank of the same aperture and thickness;

2. Raw substrates, processed substrates having surface coatings (single-layer or multi-layer, metallic or dielectric, conducting, semiconducting or insulating) or having protective films;

3. Segments or assemblies of mirrors designed to be assembled in space into an optical system with a collecting aperture equivalent to or larger than a single optic 1 m in diameter;

4. Components manufactured from composite materials having a coefficient of linear thermal expansion equal to or less than 5 × 10– 6 in any coordinate direction.

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: Item 2 above does not apply to 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:

3. a.

Single transverse mode output and output power exceeding 50 W; or

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:

5. a.

Single transverse mode output and output power exceeding 50 W; or

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:

6. a.

Single transverse mode and output power exceeding 500 W; or

Multiple transverse mode output and any of the following:

1. Wall-plug efficiency exceeding 18 % and output power exceeding 500 W; or

2. Output power exceeding 2 kW;

IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2.

(a) Output power exceeding 500 W but not exceeding 1 kW and having all of the following:

(a)

1. Beam Parameter Product (BPP) exceeding 0,7 mm · mrad; and

2. 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 · 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; or

(i) Output power exceeding 8 kW but not exceeding 10 kW and having a BPP exceeding 24 mm · mrad;

IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2. Technical note:

1. Output wavelength less than 600 nm and any of the following: Note: Item 1. above does not apply to 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. a.

Output energy exceeding 50 mJ per pulse and peak power exceeding 1 W; or

Average or CW output power exceeding 1 W;

1. Output energy less than 1,5 J per pulse or a peak power less than 20 W; and

2. 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:

2. a.

Output energy exceeding 1 J per pulse and peak power exceeding 20 W; or

Average or CW output power exceeding 20 W; or

3. Output wavelength exceeding 1400 nm and any of the following:

3. a.

Output energy exceeding 50 mJ per pulse and peak power exceeding 1 W; or

Average or CW output power exceeding 1 W;

IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2. Technical note: Notes: 1.2. 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; or

2. Wavelength greater than 1510 nm and average or CW output power, exceeding 500 mW;

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 15 W;

2. Wavelength equal to or greater than 1400 nm and less than 1900 nm and average or CW output power, exceeding 2,5 W; or

3. Wavelength equal to or greater than 1900 nm and average or CW output power, exceeding 1 W;

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; or

3. Wavelength equal to or greater than 1900 nm and average or CW output power, exceeding 10 W;

Semiconductor laser stacked arrays (two-dimensional arrays) having any of the following:

1. Wavelength less than 1400 nm and having any of the following:

1. a.

Average or CW total output power less than 3 kW and having average or CW output power density greater than 500 W/cm2;

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 350W/cm2;

Average or CW total output power exceeding 5 kW;

Peak pulsed power density exceeding 2500 W/cm2; or Note: Item d. does not apply to epitaxially fabricated monolithic devices.

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:

2. a.

Average or CW total output power less than 250 W and average or CW output power density greater than 150 W/cm2;

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 50W/cm2;

Average or CW total output power exceeding 500 W;

Peak pulsed power density exceeding 500 W/cm2; or Note: Item d. does not apply to epitaxially fabricated monolithic devices.

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:

3. a.

Average or CW output power density greater than 50 W/cm2;

Average or CW output power greater than 10 W; or

Spatially coherent average or CW total output power, exceeding 1,5W; or

4. At least one laser bar specified above;

IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2. Technical note: Notes: 1.2. Technical note: a.

Hydrogen Fluoride (HF) lasers;

Deuterium Fluoride (DF) lasers;

Transfer lasers, as follows:

1. Oxygen Iodine (O2-I) lasers;

2. Deuterium Fluoride-Carbon dioxide (DF-CO2) lasers;

3. Non-repetitive pulsed Nd: glass lasers having any of the following:

3. a.

Pulse duration not exceeding 1 μs and output energy exceeding 50 J per pulse; or

Pulse duration exceeding 1 μs and output energy exceeding 100 J per pulse;

1. Technical note:

Mirrors cooled either by active cooling or by heat pipe cooling; 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;

3. Fibre laser components:

3. 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; and

2. Number of input fibres equal to or greater than 3;

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; and

3. Having any of the following:

3. 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; or

A BPP measured at the output not exceeding 2,5 mm mrad for a number of input fibres greater than 5;

MLDs having all of the following:

1. Designed for spectral or coherent beam combination of 5 or more fibre lasers; and

2. CW Laser Induced Damage Threshold (LIDT) greater than or equal to 10 kW/cm2.

(a) Gravity meters designed or modified for ground use and having a static accuracy of less (better) than 10 μGal; Note: Item (a) does not apply to ground gravity meters of the quartz element (Worden) type.

(b) Gravity meters designed for mobile platforms and having all of the following: Technical note: For the purposes of item (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.

(b)

1. A static accuracy of less (better) than 0,7 mGal; and

2. 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;

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 International Civil Aviation Organization (ICAO) standards and employing electronically steerable linear (one-dimensional) arrays or mechanically positioned passive antennae.

IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2. Technical note: Notes: 1.2. Technical note: 1.

(a) Operating at frequencies from 40 GHz to 230 GHz and having any of the following:

(a)

1. An average output power exceeding 100 mW; or

2. Locating accuracy of 1 m or less (better) in range and 0,2 degree or less (better) in azimuth;

(b) Technical note:

A tunable bandwidth exceeding ± 6,25 % of the centre operating frequency; The centre operating frequency equals one half of the sum of the highest plus the lowest specified operating frequencies.

(d) Capable of operating in synthetic aperture radar (SAR), inverse synthetic aperture radar (ISAR) or side-looking airborne radar (SLAR) mode;

(e) Incorporating electronically steerable array antennae;

(f) Capable of height-finding non-cooperative targets;

(g) Specially designed for airborne (balloon or airframe mounted) operation and having Doppler signal processing for the detection of moving targets;

(h) Employing processing of radar signals and using any of the following:

(h)

1. Radar spread spectrum techniques; or

2. Radar frequency agility techniques;

(i) Providing ground-based operation with a maximum instrumented range exceeding 185 km; Note: Item (i) above does not apply to:

(i)

(a) Fishing ground surveillance radar;

(b) Ground radar equipment specially designed for en-route air traffic control and having all of the following:

(b)

1. A maximum instrumented range of 500 km or less;

2. Configured so that radar target data can be transmitted only one way from the radar site to one or more civil ATC centres;

3. Contains no provisions for remote control of the radar scan rate from the en-route ATC centre; and

4. Permanently installed.

(j) Notes: 1.2.3.

Being laser radar or Light Detection and Ranging (LIDAR) equipment and having any of the following: LIDAR equipment specially designed for surveying is only specified by 3. The item above does not apply to LIDAR equipment specially designed for meteorological observation. Parameters in the IHO Order 1a Standard (5th Edition, February 2008) are summarized as follows:

(j)

1. Space-qualified;

2. Employing coherent heterodyne or homodyne detection techniques and having an angular resolution of less (better) than 20 μrad (microradians); or

3. Designed for carrying out airborne bathymetric littoral surveys to International Hydrographic Organization (IHO) Order 1a Standard (5th Edition, February 2008) for Hydrographic Surveys or better, and using one or more lasers with a wavelength exceeding 400 nm but not exceeding 600 nm;

Horizontal Accuracy (95 % confidence level) = 5 m + 5 % of depth.

Depth Accuracy for Reduced Depths (95 % confidence level) = ± √(a2+ (b * d)2) where:

a = 0,5 m = constant-depth error, i.e., the sum of all constant-depth errors

b = 0,013 = factor of depth-dependent error

b * d = depth-dependent error, i.e., the sum of all depth-dependent errors

d = depth

Feature Detection = Cubic features > 2 m in depths up to 40 m; 10 % of depth beyond 40 m.

(k) Having signal processing subsystems using pulse compression and having any of the following: Note: Item 2. above does not apply to two-dimensional marine radar or vessel traffic service radar, having all of the following:

(k)

1. A pulse compression ratio exceeding 150; or

2. A compressed pulse width of less than 200 ns; or

(a) Pulse compression ratio not exceeding 150;

(b) Compressed pulse width of greater than 30 ns;

(d) Peak output power not exceeding 250 W; and

(e) Not capable of frequency hopping.

(l) Having data processing subsystems and having any of the following:

(l)

1. Automatic target tracking providing, at any antenna rotation, the predicted target position beyond the time of the next antenna beam passage; or Note: The item above does not apply to conflict alert capability in ATC systems, or marine radar.

2. Technical notes: 1.2.

Configured to provide superposition and correlation, or fusion, of target data within six seconds from two or more geographically dispersed radar sensors to improve the aggregate performance beyond that of any single sensor specified in items (f) or (i). Note: The item above does not apply to systems, equipment and assemblies used for vessel traffic services. For the purposes of this section, marine radar is a radar that is used to navigate safely at sea, in inland waterways or in near-shore environments. For the purposes of this section, vessel traffic service is a vessel traffic monitoring and control service similar to air traffic control for aircraft.

(a) Equipment for measuring absolute reflectance to an accuracy of equal to or better than 0,1 % of the reflectance value;

(b) Equipment other than optical surface scattering measurement equipment, having an unobscured aperture of more than 10 cm, specially designed for the non-contact optical measurement of a non-planar optical surface figure (profile) to an accuracy of 2 nm or less (better) against the required profile.

(a) Elemental tellurium (Te) of purity levels of 99,9995 % or more;

(b) Single crystals (including epitaxial wafers) of any of the following:

(b)

1. Cadmium zinc telluride (CdZnTe) with zinc content of less than 6 % by mole fraction;

2. Cadmium telluride (CdTe) of any purity level; or

3. Mercury cadmium telluride (HgCdTe) of any purity level.

IX.A6. Technical notes: 1.2. Notes: 1.2.3. Notes: 1.2. Technical note: Notes: 1.2. Technical note: 1. Technical note:

(a) Zinc selenide (ZnSe) and zinc sulphide (ZnS) substrate blanks, produced by the chemical vapour deposition process and having any of the following:

(a)

1. A volume greater than 100 cm3; or

2. A diameter greater than 80 mm and a thickness of 20 mm or more;

(b) Electro-optic materials and non-linear optical materials, as follows:

(b)

1. Potassium titanyl arsenate (KTA) (CAS 59400-80-5);

2. Silver gallium selenide (AgGaSe2, also known as AGSE) (CAS 12002-67-4);

3. Thallium arsenic selenide (Tl3AsSe3, also known as TAS) (CAS 16142-89-5);

4. Zinc germanium phosphide (ZnGeP2, also known as ZGP, zinc germanium biphosphide or zinc germanium diphosphide); or

5. Gallium selenide (GaSe) (CAS 12024-11-2);

1. A hydroxyl ion (OH–) concentration of less than 5 ppm;

2. Integrated metallic purity levels of less than 1 ppm; and

3. High homogeneity (index of refraction variance) less than 5 × 10– 6;

(e) Synthetically produced diamond material with an absorption of less than 10– 5 cm– 1 for wavelengths exceeding 200 nm but not exceeding 14000 nm.

(a) Synthetic crystalline laser host material in unfinished form as follows:

(a)

1. Titanium doped sapphire;

(b) Rare-earth-metal doped double-clad fibres;

(b)

1. Nominal laser wavelength of 975 nm to 1150 nm and having all of the following: Note: The item above does not apply to double-clad fibres having an inner glass cladding diameter exceeding 150 μm and not exceeding 300 μm.

1. a.

Average core diameter equal to or greater than 25 μm; and

Core Numerical Aperture (NA) less than 0,065; or

2. Nominal laser wavelength exceeding 1530 nm and having all of the following:

2. a.

Average core diameter equal to or greater than 20 μm; and

Core NA less than 0,1.

IX.A7. Technical note: Technical note:

NAVIGATION AND AVIONICS No Description Related item from Annex I to Regulation (EC) No 428/2009 IX.A7.001 Star trackers and components therefor, as follows: Star trackers are also referred to as stellar attitude sensors or gyro-astro compasses. 7A004 IX.A7.002 Global Navigation Satellite Systems (GNSS) receiving equipment having any of the following and specially designed components therefor: Note: Item (b) does not apply to 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. For the purposes of item (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. 7A005 IX.A7.003 Airborne altimeters operating at frequencies other than 4,2 to 4,4 GHz inclusive and having any of the following: 7A006 IX.A7.004 Test, calibration or alignment equipment, specially designed for equipment specified in the section above. 7B001 IX.A7.005 Equipment specially designed to characterize mirrors for ring laser gyros, as follows: 7B002 IX.A7.006 Equipment specially designed for the production of equipment specified IN IX.A7. Note: Including: 7B003

IX.A7.

(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 item (a), as follows:

(b)

1. Optical heads or baffles;

2. Data processing units.

IX.A7. Technical note:

(a) Employing a decryption algorithm specially designed or modified for government use to access the ranging code for position and time; or

(b) Employing adaptive antenna systems.

IX.A7. Technical note: Technical note:

(a) Power management; or

(b) Using phase shift key modulation.

(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).

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.

IX.A8. Technical note:

MARINE No Description Related item from Annex I to Regulation (EC) No 428/2009 IX.A8.001 Systems, equipment and components, specially designed or modified for submersible vehicles and designed to operate at depths exceeding 1000 m, as follows: 8A002.a. IX.A8.002 Systems specially designed or modified for the automated control of the motion of submersible vehicles specified above, using navigation data, having closed loop servo-controls and having any of the following: 8A002.b. IX.A8.003 Fibre-optic pressure hull penetrators; 8A002.c. IX.A8.004 Robots specially designed for underwater use, controlled by using a dedicated computer and having any of the following: 8A002.h. IX.A8.005 Stirling cycle engine air independent power systems having all of the following: 8A002.j. IX.A8.006 Noise reduction systems designed for use on vessels of 1000 tonnes displacement or more, as follows: Active noise reduction or cancellation systems incorporate electronic control systems capable of actively reducing equipment vibration by the generation of anti-noise or anti-vibration signals directly to the source. 8A002.j.

IX.A8.

1. Pressure housings or pressure hulls with a maximum inside chamber diameter exceeding 1,5 m;

2. Direct current propulsion motors or thrusters;

3. Umbilical cables, and connectors therefor, using optical fibre and having synthetic strength members;

4. Components manufactured from material as follows: Syntactic foam designed for underwater use and having all of the following:

4. a.

Designed for marine depths exceeding 1000 m; and

A density less than 561 kg/m3;

1. Enabling a vehicle to move within 10 m of a predetermined point in the water column;

2. Maintaining the position of the vehicle within 10 m of a predetermined point in the water column; or

3. Maintaining the position of the vehicle within 10 m while following a cable on or under the seabed;

(a) Systems that control the robot using information from sensors which measure force or torque applied to an external object, distance to an external object, or tactile sense between the robot and an external object; or

(b) The ability to exert a force of 250 N or more or a torque of 250 Nm or more and using titanium-based alloys or composite fibrous or filamentary materials in their structural members;

(a) Devices or enclosures, specially designed for underwater noise reduction in frequencies below 10 kHz, or special mounting devices for shock mitigation; and

(b) Specially designed exhaust systems which discharge the products of combustion against a pressure of 100 kPa or more;

(a) Systems that attenuate underwater noise at frequencies below 500 Hz and consist of compound acoustic mounts for the acoustic isolation of diesel engines, diesel generator sets, gas turbines, gas turbine generator sets, propulsion motors or propulsion reduction gears, specially designed for sound or vibration isolation and having an intermediate mass exceeding 30 % of the equipment to be mounted;

(b) Active noise reduction or cancellation systems or magnetic bearings, specially designed for power transmission systems.

IX.A9. AEROSPACE AND PROPULSION No Description Related item from Annex I to Regulation (EC) No 428/2009 IX.A9.001 Aero gas turbine engines: 9A001 IX.A9.002 Marine gas turbine engines with an ISO standard continuous power rating of 24245 kW or more and a specific fuel consumption not exceeding 0,219 kg/kWh in the power range from 35 to 100 %, and specially designed assemblies and components therefor. Note: The term marine gas turbine engines includes those industrial, or aero-derivative, gas turbine engines adapted for a ship's electric power generation or propulsion. 9A002 IX.A9.003 Specially designed assemblies or components, incorporating any of the technologies specified in paragraph 2 of the section below entitled Technology, for any of the following aero gas turbine engines: 9A003 IX.A9.004 Space launch vehicles, spacecraft, spacecraft buses, spacecraft payloads, spacecraft on-board systems or equipment, and terrestrial equipment, as follows: 9A004 IX.A9.005 Liquid rocket propulsion systems. 9A005 IX.A9.006 Systems and components, specially designed for liquid rocket propulsion systems, as follows: 9A006 IX.A9.007 Solid rocket propulsion systems. 9A007 IX.A9.008 Components specially designed for solid rocket propulsion systems, as follows: 9A008 IX.A9.009 Hybrid rocket propulsion systems. 9A009 IX.A9.010 Specially designed components, systems and structures, for launch vehicles, launch vehicle propulsion systems or spacecraft, as follows: 9A010 IX.A9.011 Unmanned Aerial Vehicles (UAVs), unmanned airships, related equipment and components, as follows: 9A012 IX.A9.012 On-line (real-time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment specially designed for the development of gas turbine engines, assemblies or components and incorporating any of the technologies specified in paragraph 2 (b) or 2 (c) of the section below entitled Technology. 9B002 IX.A9.013 Equipment specially designed for the production or test of gas turbine brush seals designed to operate at tip speeds exceeding 335 m/s and temperatures in excess of 773 K (500 °C), and specially designed components or accessories therefor. 9B003 IX.A9.014 Tools, dies or fixtures, for the solid-state joining of superalloy, titanium or intermetallic airfoil-to-disk combinations described in paragraph 2 of the section below entitled Technology for gas turbines. 9B004 IX.A9.015 On-line (real-time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use in wind tunnels designed for speeds of Mach 1,2 or more. 9B005 IX.A9.016 Acoustic vibration test equipment capable of producing sound pressure levels of 160 dB or more (referenced to 20 Pa) 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. 9B006 IX.A9.017 Equipment specially designed for inspecting the integrity of rocket motors and using Non-Destructive Test (NDT) techniques other than planar X-ray or basic physical or chemical analysis. 9B007 IX.A9.018 Direct measurement wall skin friction transducers specially designed to operate at a test flow total (stagnation) temperature exceeding 833 K (560 °C). 9B008 IX.A9.019 Tooling specially designed for producing gas turbine engine powder metallurgy rotor components having all of the following: Note: The item above does not specify tooling for the production of powder. 9B008 IX.A9.020 Equipment specially designed for the production of items specified by Unmanned Aerial Vehicles (UAVs), unmanned airships and components. 9B010

IX.A9.

(a) Incorporating any of the technologies specified in paragraph 2 of the section below entitled Technology; or Note 1: This item does not apply to aero gas turbine engines which meet all of the following: Note 2: This item does not apply to aero gas turbine engines designed for Auxiliary Power Units (APUs) approved by the civil aviation authority of the Member State.

(a)

(a) Certified by civil aviation authorities; and

(b) Intended to power non-military manned aircraft for which any of the following has been issued by civil aviation authorities for the aircraft with this specific engine type:

(b)

1. A civil type certificate; or

2. An equivalent document recognized by ICAO.

(b) Designed to power an aircraft designed to cruise at Mach 1 or higher, for more than 30 minutes.

(a) Specified in item 1 above; or

(b) Whose design or production origins are unknown to the manufacturer.

(a) Space launch vehicles;

(b) Spacecraft;

(d) Spacecraft payloads incorporating items specified in this list;

(e) On-board systems or equipment, specially designed for spacecraft and having any of the following functions:

(e)

1. Command and telemetry data handling;

(f) Terrestrial equipment specially designed for spacecraft, as follows:

(f)

1. Telemetry and telecommand equipment;

2. Simulators.

(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;

(d) High-pressure (exceeding 17,5 MPa) turbo pumps, pump components or their associated gas generator or expander cycle turbine drive systems;

(e) High-pressure (exceeding 10,6 MPa) thrust chambers and nozzles therefor;

(f) Propellant storage systems using the principle of capillary containment or positive expulsion (i.e., with flexible bladders);

(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;

(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

(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;

(b) Technical note:

Filament-wound composite motor cases exceeding 0,61 m in diameter or having structural efficiency ratios (PV/W) exceeding 25 km; Structural efficiency ratio (PV/W) is the burst pressure (P) multiplied by the vessel volume (V) divided by the total pressure vessel weight (W).

(d) Movable nozzle or secondary fluid injection thrust vector control systems, capable of any of the following:

(d)

1. Omni-axial movement exceeding ± 5°;

2. Angular vector rotations of 20°/s or more; or

3. Angular vector accelerations of 40°/s2 or more.

(a) Components and structures, specially designed for launch vehicle propulsion systems manufactured using any of the following:

(a)

1. Fibrous or filamentary materials;

2. Metal matrix composite materials; or

3. Ceramic matrix composite materials.

(a) Technical notes: 1.2.3.

UAVs or unmanned airships, designed to have controlled flight out of the direct natural vision of the operator and having any of the following: For the purposes of the item above, operator is a person who initiates or commands the UAV or unmanned airship flight. For the purposes of the item above, endurance is to be calculated for International Standard Atmosphere (ISA) conditions (ISO 2533:1975) at sea level in zero wind. For the purposes of the item above, natural vision means unaided human sight, with or without corrective lenses.

(a)

1. Having all of the following:

1. a.

A maximum endurance greater than or equal to 30 minutes but less than 1 hour; and

Designed to take off and have stable controlled flight in wind gusts equal to or exceeding 46,3 km/h (25 knots); or

2. A maximum endurance of 1 hour or greater;

(b) Related equipment and components, as follows:

(b)

1. Equipment or components, specially designed to convert a manned aircraft or a manned airship to a UAV or unmanned airship, specified in item (a) above;

2. 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).

(a) Designed to operate at stress levels of 60 % of ultimate tensile strength (UTS) or more measured at a temperature of 873 K (600 °C); and

(b) Designed to operate at 873 K (600 °C) or more.

SOFTWARE No Description Related item from Annex I to Regulation (EC) No 428/2009 IX.B.001 Software specially designed or modified for the development, production or use of equipment specified in IX.A1. 1D001 1D002 1D003 IX.B.002 Software for the development of material specified in IX.A1. 1D001 1D002 1D003 IX.B.003 Software specially designed or modified to enable non-listed equipment to perform the functions of any equipment specified in IX.A1. 1D001 1D002 1D003 IX.B.004 Software specially designed or modified for the development, production or use of equipment specified in IX.A2 2D001 IX.B.005 Software specially designed or modified to allow non-listed equipment to function as equipment specified IX.A2 2D003 2D101 2D202 IX.B.006 Software specially designed for the development, production or use of equipment specified in IX.A3. 3D001 3D002 3D003 IX.B.007 Software specially designed or modified to allow non-listed equipment to function as equipment specified in IX.A3 3D001 3D002 3D003 IX.B.008 Software specially designed for the development, production or use of equipment specified in IX.A6. 6D001 6D003 6D002 6D102 6D203 6D203 IX.B.009 Software specially designed or modified to allow non-listed equipment to function as equipment specified in IX.A6. 6D001 6D003 6D002 6D102 6D203 6D203 IX.B.010 Software specially designed or modified for the development, production or use of equipment specified in IX.A7. 7D001 7D002 7D003 7D004 7D005 7D102 7D103 7D104 IX.B.011 Software specially designed or modified to allow non-listed equipment to function as equipment specified IX.A7. 7D001 7D002 7D003 7D004 7D005 7D102 7D103 7D104 IX.B.012 Source code for the operation or maintenance of equipment specified IX.A7. 7D001 7D002 7D003 7D004 7D005 7D102 7D103 7D104 IX.B.013 Computer-Aided Design (CAD) software specially designed for the development of active flight control systems, helicopter multi-axis fly-by-wire or fly-by-light controllers or helicopter circulation controlled anti-torque or circulation-controlled direction control systems. 7D001 7D002 7D003 7D004 7D005 7D102 7D103 7D104 IX.B.014 Software specially designed or9modified for the development, production or use of equipment. Specified in IX.A9. 9D001 9D002 9D003 9D004 9D005 9D101 9D103 9D104 9D105 IX.B.015 Software specially designed or modified to allow non-listed equipment to function as equipment specified in IX.A9. 9D001 9D002 9D003 9D004 9D005 9D101 9D103 9D104 9D105

TECHNOLOGY No Description Related item from Annex I to Regulation (EC) No 428/2009 IX.C.001 Technology for the development, production or use of equipment or software specified in IX.A1. 2E001 IX.C.002 Technology for the development, production or use of equipment or materials specified in IX.A3 3E001 3E003 3E101 3E102 3E201 IX.C.003 Technology for the development, production and use of equipment or software, specified in IX.A7. 7E001 7E002 7E003 7E004 7D005 7E101 7E102 7E104 IX.C.004 Technology for the development, production or use of equipment or software, specified in IX.A9. 9E001 9E002 IX.C.005 Other technology, as follows: 9E003.a. IX.C.006 Technology for gas turbine engine Full Authority Digital Engine Control (FADEC) systems, as follows: Note: Item (b) above does not apply to technical data related to engine-aircraft integration required by civil aviation authorities of one or more Member States to be published for general airline use (e.g., installation manuals, operating instructions, instructions for continued airworthiness) or interface functions (e.g., input/output processing, airframe thrust or shaft power demand). 9E003.h. IX.C.007 Technology for adjustable flow path systems designed to maintain engine stability for gas generator turbines, fan or power turbines, or propelling nozzles, as follows: 9E003.i

(a) Technology required for the development or production of any of the following gas turbine engine components or systems:

(a)

1. Gas turbine blades, vanes or tip shrouds, made from directionally solidified (DS) or single crystal (SC) alloys and having (in the 001 Miller Index Direction) a stress-rupture life exceeding 400 hours at 1273 K (1000 °C) at a stress of 200 MPa, based on the average property values;

2. Combustors having any of the following:

2. a.

Thermally decoupled liners designed to operate at combustor exit temperature exceeding 1883 K (1610 °C);

Non-metallic liners;

Non-metallic shells; or

Liners designed to operate at combustor exit temperature exceeding 1883 K (1610 °C) and having holes that meet the parameters specified by 9E003.c.;

3. Components that are any of the following:

3. a.

Manufactured from organic composite materials designed to operate above 588 K (315 °C);

Manufactured from any of the following:

1. Metal matrix composites; or

2. Ceramic matrix composites; or

Stators, vanes, blades, tip seals (shrouds), rotating blings, rotating blisks, or splitter ducts, that are all of the following:

1. Not specified above;

2. Designed for compressors or fans; and

3. Manufactured from material fibrous or filamentary materials with resins;

4. Uncooled turbine blades, vanes or tip-shrouds, designed to operate at a gas path temperature of 1373 K (1100 °C) or more;

5. Cooled turbine blades, vanes, tip-shrouds, designed to operate at a gas path temperature of 1693 K (1420 °C) or more;

6. Airfoil-to-disk blade combinations using solid-state joining;

7. Gas turbine engine components using diffusion bonding technology;

8. Damage tolerant gas turbine engine rotor components using powder metallurgy materials;

9. Hollow fan blades.

1. Development technology for deriving the functional requirements for the components necessary for the FADEC system to regulate engine thrust or shaft power (e.g., feedback sensor time constants and accuracies, fuel valve slew rate);

2. Development or production technology for control and diagnostic components unique to the FADEC system and used to regulate engine thrust or shaft power;

3. Development technology for the control law algorithms, including source code, unique to the FADEC system and used to regulate engine thrust or shaft power;

1. Development technology for deriving the functional requirements for the components that maintain engine stability;

2. Development or production technology for components unique to the adjustable flow path system and that maintain engine stability;

3. Development technology for the control law algorithms, including source code, unique to the adjustable flow path system and that maintain engine stability

Versions

2019-06-21