LegalizeCouncil Regulation (EU) 2017/1509 of 30 August 2017 concerning restrictive measures against the Democratic People's Republic of Korea and repealing Regulation (EC) No 329/2007
| 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: Note: 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: — An area not exceeding 1 m2; — A length not exceeding 2,5 m; — A width exceeding 15 mm. 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. (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 1 649 °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 1 770 °C in an inert environment. (b) ‘Fibrous or filamentary materials’ having any of the following: 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: 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. b. Carbon ‘fibrous or filamentary materials’, having a ‘specific modulus’ exceeding 14,65 × 106 m; and specific tensile strength exceeding 26,82 × 104 m. c. Inorganic ‘fibrous or filamentary materials’, having a ‘specific modulus’ exceeding 2,54 × 106 m; and a melting, softening, decomposition or sublimation point exceeding 1 649 °C in an inert environment. Notes: 1. Does not apply to polyethylene. 2. Does not apply to — ‘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. 3. 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 1 770 °C in an inert environment. (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) 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: 1. Inorganic ‘fibrous or filamentary materials’ with a ‘specific modulus’ exceeding 2,54 × 106 m and a melting, softening, decomposition or sublimation point exceeding 1 649 °C in an inert environment, or 2. Organic or carbon ‘fibrous or filamentary materials’, having all of the following: a. ‘Specific modulus’ exceeding 10,15 × 106 m; and b. ‘Specific tensile strength’ exceeding 17,7 × 104 m; or 3. Resin or pitch, from unprocessed fluorinated compounds such as: 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; 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. Note: Does not apply to — 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 | 1A002 1A202 |
| VII.A1.002 | ‘Fibrous or filamentary materials’ having any of the following: (a) Materials composed of aromatic polyetherimides having a glass transition temperature (Tg) exceeding 290 °C. (b) Polyarylene ketones. (c) Polyarylene sulphides where the arlylene group is biphenylene, triphenylene or combinations thereof (d) Polybiphenylenethersulphone having a Tg exceeding 290 °C, or (e) Any of the above materials commingled with any of the following: 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 1 649 °C in an inert environment. Notes: 1. Does not apply to polyethylene. 2. Does not apply to: — ‘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. 3. 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 1 770 °C in an inert environment | 1C008 1C010 1C210 9C110 |
| VII.A1.003 | Equipment for the ‘production’ or inspection of ‘composite’ structures Specially designed components and accessories to include: (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: 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: a. X-ray tomography systems for three dimensional defect inspection; b. 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. Notes: 1. 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. 2. The technique of interlacing includes knitting. | 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: (a) Aluminides, including: 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: 1. Nickel alloys having a stress-rupture life of 10 000 hours or longer at 650 °C at a stress of 676 MPa or a low cycle fatigue life of 10 000 cycles or more at 550 °C at a maximum stress of 1 095 MPa; 2. Niobium alloys having a stress-rupture life of 10 000 hours or longer at 800 °C at a stress of 400 MPa or a low cycle fatigue life of 10 000 cycles or more at 700 °C at a maximum stress of 700 MPa; 3. Titanium alloys having a stress-rupture life' of 10 000 hours or longer at 450 °C at a stress of 200 MPa or a low cycle fatigue life of 10 000 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: 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 b. Niobium alloys (Nb-Al-X or Nb-X-Al, Nb-Si-X or Nb-X-Si, Nb Ti X or Nb-X-Ti) c. Titanium alloys (Ti-Al-X or Ti-X-Al) d. Aluminium alloys (Al-Mg-X or Al-X-Mg, Al-Zn-X or Al-X-Zn, Al Fe-X or Al-X-Fe) or e. Magnesium alloys (Mg-Al-X or Mg-X-Al) 7. Made in a controlled environment by any of the following processes: a. ‘Vacuum atomization’ b. ‘Gas atomization’ c. ‘Rotary atomization’ d. ‘Splat quenching’ e. ‘Melt spinning and comminution’ Note: 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: (a) Initial relative permeability of 120 000 or more and a thickness of 0,5 mm or less (b) Magnetostrictive alloys having any of the following: 1. A saturation magnetostriction of more than 5 × 10– 4; or 2. A magnetomechanical coupling factor (k) of more than 0,8; or (c) Amorphous or ‘nanocrystalline’ alloy strips, having all of the following: 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: a. A strip thickness of 0,02 mm or less; or b. An electrical resistivity of 2 × 10– 4 ohm cm or more. | 1C003 |
| VII.A1.006 | Uranium titanium alloys or tungsten alloys with a ‘matrix’ based on iron, nickel or copper, having all of the following: (a) A density exceeding 17,5 g/cm3; (b) An elastic limit exceeding 880 MPa; (c) An ultimate tensile strength exceeding 1 270 MPa; and (d) An elongation exceeding 8 %. | 1C004 |
| VII.A1.007 | ‘Superconductive’ composite conductors in lengths exceeding 100 m or with a mass exceeding 100 g, as follows: (a) ‘Superconductive’‘composite’ conductors containing one or more niobium-titanium ‘filaments’, having all of the following: 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: 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 1 750 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 | 1C005 |
| VII.A1.008 | Fluids and lubricating materials, as follows: (a) Lubricating materials containing, as their principal ingredients, any of the following: 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 5 000 mm2/s (5 000 centistokes) measured at 25 °C; (b) Damping or flotation fluids having all of the following: 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: a. Dibromotetrafluoroethane (CAS 25497-30-7, 124-73-2, 27336-23-8); b. Polychlorotrifluoroethylene (oily and waxy modifications only); or c. Polybromotrifluoroethylene (c) Fluorocarbon electronic cooling fluids having all of the following: 1. Containing 85 % by weight or more of any of the following, or mixtures thereof: a. Monomeric forms of perfluoropolyalkylether-triazines or perfluoroaliphatic-ethers; b. Perfluoroalkylamines; c. Perfluorocycloalkanes; or d. Perfluoroalkanes e. Density at 298 K (25 °C) of 1,5 g/ml or more; f. In a liquid state at 273 K (0 °C); and g. Containing 60 % or more by weight of fluorine 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: (a) Ceramic powders of single or complex borides of titanium, having total metallic impurities, excluding intentional additions, of less than 5 000 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: 1. Made from any of the following materials: a. Si-N; b. Si-C; c. Si-A1-O-N; or d. 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: 1. Polydiorganosilanes (for producing silicon carbide); 2. Polysilazanes (for producing silicon nitride); 3. Polycarbosilazanes (for producing ceramics with silicon, carbon and nitrogen components); (f) Ceramic-ceramic ‘composite’ materials with an oxide or glass ‘matrix’ reinforced with continuous fibres from any of the following systems: 1. Al2O3 (CAS 1344-28-1); or 2. Si-C-N. Notes: 1. Does not apply to abrasives. 2. Does not apply to ‘composites’ containing fibres from these systems with a fibre ‘tensile strength’ of less than 700 MPa at 1 273 K (1 000 °C) or fibre tensile creep resistance of more than 1 per cent creep strain at 100 MPa load and 1 273 K (1 000 °C) for 100 hours. | 1C007 |
| VII.A1.010 | Non-fluorinated polymeric substances as follows: (a) Imides as follows: 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; (c) Polyarylene sulphides, where the arylene group is biphenylene, triphenylene or combinations thereof; (d) Polybiphenylenethersulphone having a ‘glass transition temperature (Tg)’ exceeding 290°C. 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: (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. | 1C009 |
| VII.A1.012 | ‘Fibrous or filamentary materials’ as follows: (a) Organic ‘fibrous or filamentary materials’, having all of the following: 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: 1. ‘specific modulus’ exceeding 14,65 × 106 m; and 2. ‘specific tensile strength’ exceeding 26,82 × 104 m; (c) Inorganic ‘fibrous or filamentary materials’, having all of the following: 1. ‘Specific modulus’ exceeding 2,54 × 106 m; and 2. Melting, softening, decomposition or sublimation point exceeding 1 649 °C in an inert environment (d) ‘Fibrous or filamentary materials’, having any of the following: 1. Composed of any of the following: a. Polyetherimides specified in VII.A1.010 b. 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: 1. Having any of the following: a. Inorganic ‘fibrous or filamentary materials’ specified above b. 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: a. Resin or pitch, specified in previous sections; b. ‘Dynamic Mechanical Analysis glass transition temperature (DMA Tg)’ equal to or exceeding 180 °C and having a phenolic resin; or c. ‘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. Notes: 1. Does not apply to polyethylene. 2. Does not apply to ‘fibrous or filamentary materials’, for the repair of ‘civil aircraft’ structures or laminates, having all of the following: (a) An area not exceeding 1 m2; (b) A length not exceeding 2,5 m; 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. 3. Does not apply to the following: (a) Discontinuous, multiphase, polycrystalline alumina fibres in chopped fibre or random mat form, containing 3 % by weight or more silica, with a ‘specific modulus’ of less than 10 × 106 m; (b) Molybdenum and molybdenum alloy fibres; (c) Boron fibres; (d) Discontinuous ceramic fibres with a melting, softening, decomposition or sublimation point lower than 2 043 K (1 770 °C) in an inert environment. 4. Does not apply to: (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; 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. | 1C010.a. 1C010.b. 1C010.c. |
| VII.A1.013 | Metals and compounds, as follows: (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: 1. Boron with a purity of 85 % by weight or more; 2. Boron alloys with a boron content of 85 % by weight or more; (c) Guanidine nitrate (CAS 506-93-4); (d) Nitroguanidine (NQ) (CAS 556-88-7) 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: (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. 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 |
| 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: (a) Specially designed to have any of the following: 1. Radiation hardened to exceed any of the following specifications: a. Total dose 5 × 103 Gy (Si); b. Dose rate upset 5 × 106 Gy (Si)/s; or c. Single event upset 1 × 10– 8 error/bit/day. | 4A001 |
| 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: (a) Specially designed to have any of the following: 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. Note: Does not apply to radio equipment specially designed for use with any of the following: (a) Civil cellular radio-communications systems; or (b) Fixed or mobile satellite earth stations for commercial civil telecommunications. (b) Being digitally controlled radio receivers having all of the following: 1. More than 1 000 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. Note: Does not apply to radio equipment specially designed for use with civil cellular radio-communications systems. Technical note: ‘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. | 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 |
| No | Description | Related item from Annex I to Regulation (EC) No 428/2009 |
| --- | --- | --- |
| VII.A6.001 | Hydrophones having any of the following: (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) Having any of the following sensing elements: 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 1 000 m. 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: (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; (c) Heading sensors specified in VII.A6.003 (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: 1. Composed of three accelerometers arranged along three distinct axes; 2. Having an overall ‘acceleration sensitivity’ better than 48 dB (reference 1 000 mV rms per 1g); 3. Designed to operate at depths greater than 35 metres; and 4. Operating frequency below 20 kHz. | 6A001.a. |
| VII.A6.003 | Heading sensors having all of the following: (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; | 6A001.a. |
| VII.A6.004 | Bottom or bay-cable hydrophone arrays having any of the following: (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: 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 (c) Incorporating accelerometer based hydro-acoustic sensors. Technical note: Accelerometer-based hydro-acoustic sensors having all of the following: 1. Composed of three accelerometers arranged along three distinct axes; 2. Having an overall ‘acceleration sensitivity’ better than 48 dB (reference 1 000 mV rms per 1g); 3. Designed to operate at depths greater than 35 metres; and 4. Operating frequency below 20 kHz. Notes: 1. Does not apply to particle velocity sensors or geophones. 2. 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: (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 30 000 nm and having all the following; 1. Providing output imaging data in digital format; and 2. Having any of the following characteristics: a. ‘Space-qualified’; or b. Designed for airborne operation, using other than silicon detectors, and having an IFOV of less than 2,5 mrad (milliradians); 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’: (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’. | 6A002 |
| VII.A6.006 | ‘Space-qualified’ components for optical systems, as follows: (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; | 6A004.a. |
| VII.A6.007 | Optical control equipment as follows: (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: 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: a. A maximum angular travel of ±26 mrad or more; b. A mechanical resonant frequency of 500 Hz or more; and c. 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) Gimbals having all of the following: 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: 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 b. Exceeding 1 m in diameter or major axis length and capable of angular accelerations exceeding 0,5 rad (radians)/s2. | 6A004.d. |
| VII.A6.008 | ‘Magnetometers’ using superconductive technology (SQUID) and having any of the following: (a) SQUID systems designed for stationary operation, without specially designed subsystems designed to reduce in-motion noise, and having a ‘sensitivity’ equal to or lower (better) than 50 fT (rms) per square root Hz at a frequency of 1 Hz; 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 Except: — 6A006.a.3 "Magnetometers" using fluxgate "technology" — 6A006.a.4 Induction coil "magnetometers" — 6A006.b. Underwater electric field sensors |
| 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: (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 Note: 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 |
| No | Description | Related item from Annex I to Regulation (EC) No 428/2009 |
| --- | --- | --- |
| VII.A7.001 | Accelerometers as follows and specially designed components therefor: (a) Linear accelerometers having any of the following: 1. Specified to function at linear acceleration levels less than or equal to 15 g and having any of the following: a. A ‘bias’‘stability’ of less (better) than 130 micro g with respect to a fixed calibration value over a period of one year; or b. A ‘scale factor’‘stability’ of less (better) than 130 ppm with respect to a fixed calibration value over a period of one year; 2. Specified to function at linear acceleration levels exceeding 15 g but less than or equal to 100 g and having all of the following: a. A ‘bias’‘repeatability’ of less (better) than 1 250 micro g over a period of one year; and b. A ‘scale factor’‘repeatability’ of less (better) than 1 250 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; Note: paragraphs above do not apply to accelerometers limited to measurement of only vibration or shock. (b) Angular or rotational accelerometers, specified to function at linear acceleration levels exceeding 100 g. | 7A001 |
| VII.A7.002 | Gyros or angular rate sensors, having any of the following and specially designed components therefor: (a) Specified to function at linear acceleration levels less than or equal to 100 g and having any of the following: 1. A rate range of less than 500 degrees per second and having any of the following: a. A ‘bias’‘stability’ of less (better) than 0,5 degree per hour, when measured in a 1 g environment over a period of one month, and with respect to a fixed calibration value; or b. An ‘angle random walk’ of less (better) than or equal to 0,0035 degree per square root hour; or Note: this paragraph does not apply to ‘spinning mass gyros’. 2. A rate range greater than or equal to 500 degrees per second and having any of the following: a. A ‘bias’‘stability’ of less (better) than 4 degrees per hour, when measured in a 1 g environment over a period of three minutes, and with respect to a fixed calibration value; or b. An ‘angle random walk’ of less (better) than or equal to 0,1 degree per square root hour; or Note: this paragraph does not apply to ‘spinning mass gyros’. (b) Specified to function at linear acceleration levels exceeding 100 g. | 7A002 |
| VII.A7.003 | ‘Inertial measurement equipment or systems’, having any of the following: Notes: 1. ‘Inertial measurement equipment or systems’ incorporate accelerometers or gyroscopes to measure changes in velocity and orientation in order to determine or maintain heading or position without requiring an external reference once aligned. ‘Inertial measurement equipment or systems’ include: — Attitude and Heading Reference Systems (AHRSs); — Gyrocompasses; — Inertial Measurement Units (IMUs); — Inertial Navigation Systems (INSs); — Inertial Reference Systems (IRSs); — Inertial Reference Units (IRUs). 2. 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. (a) Designed for ‘aircraft’, land vehicles or vessels, providing position without the use of ‘positional aiding references’, and having any of the following ‘accuracies’ subsequent to normal alignment: 1. 0,8 nautical miles per hour (nm/hr) ‘Circular Error Probable’ (‘CEP’) rate or less (better); 2. 0,5 % distanced travelled ‘CEP’ or less (better); 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: 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: 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. | 7A003 |
| 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: (a) Brayton or Rankine cycle engine air independent power systems having any of the following: 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: a. Specially designed to pressurise the products of reaction or for fuel reformation; b. Specially designed to store the products of the reaction; and c. Specially designed to discharge the products of the reaction against a pressure of 100 kPa or more; | 8A002.j. |
| VII.A8.002 | Diesel cycle engine air independent systems having all of the following: (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; | 8A002.j. |
| VII.A8.003 | Fuel cell air independent power systems with an output exceeding 2kW and having any of the following: (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: 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 | 8A002.j. |
| VII.A8.004 | Stirling cycle engine air independent power systems having all of the following: (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; | 8A002.p. |
| VII.A8.005 | Manned, tethered submersible vehicles designed to operate at depths exceeding 1 000 m. | 8A001.a. |
| 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: (a) Directional solidification or single crystal casting equipment; (b) Casting tooling, manufactured from refractory metals or ceramics, as follows: 1. Cores 2. Shells (moulds) 3. Combined core and shell (mould) units (c) Directional-solidification or single-crystal additive-manufacturing equipment. | 9B001 |
| VII.A9.002 | Aero gas turbine engines, except aero gas turbine engines which meet all of the following: (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: 1. A civil type certificate; or 2. An equivalent document recognized by the International Civil Aviation Organization. | 9A001 |
| 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: (a) Machine tools for turning having two or more axes which can be coordinated simultaneously for ‘contouring control’ having any of the following: 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: 1. Three linear axes plus one rotary axis which can be coordinated simultaneously for ‘contouring control’ having any of the following: 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 b. ‘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: 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; b. ‘Unidirectional positioning repeatability’ equal to or less (better) than 1,4 μm along one or more linear axis with a travel length equal to or greater than 1 m and less than 4 m; c. ‘Unidirectional positioning repeatability’ equal to or less (better) than 6,0 μm along one or more linear axis with a travel length equal to or greater than 4 m; 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 1 250 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). | 2D001 2D002 |
| VII.B.003 | ‘Software’ for marine systems, equipment, components, test, inspection and ‘production’ equipment and other related technology | 8D001 8D002 |
| 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).
| 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 100 000 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 |
| 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 |
| 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 |
| 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: (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 | 3B002 |
| VIII.A3.005 | Chromatography and spectrometry analytical instruments | 3A233 |
| 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).
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