No | Description | Related item from Annex I to Regulation (EC) No 428/2009 |
---|
II.A1.001 | Bis(2-ethylhexyl) phosphoric acid (HDEHP or D2HPA) CAS 298-07-7 solvent in any quantity, with a purity greater than 90 %. | — |
II.A1.002 | Fluorine gas (Chemical Abstract Number (CAS): 7782-41-4), with a purity of at least 95 %. | — |
II.A1.005 | Electrolytic cells for fluorine production with an output capacity greater than 100 g of fluorine per hour.
Note: This item does not cover electrolytic cells defined in item 1B225. | 1B225 |
II.A1.006 | Catalysts, other than those prohibited by 1A225, containing platinum, palladium or rhodium, usable for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water. | 1B231, 1A225 |
II.A1.007 | Aluminium and its alloys, other than those specified in 1C002.b.4 or 1C202.a, in crude or semi-fabricated form having either of the following characteristics:
a. Capable of an ultimate tensile strength of 460 MPa or more at 293 K (20 °C); or
b. Having a tensile strength of 415 MPa or more at 298 K (25 °C).
| 1C002.b.4, 1C202.a |
II.A1.008 | Magnetic metals, of all types and of whatever form, having an initial relative permeability of 120 000 or more and a thickness between 0,05 and 0,1 mm. | 1C003.a |
II.A1.009 | 'Fibrous or filamentary materials' or prepregs, as follows:
N.B. SEE ALSO II.A1.019.A. a. Carbon or aramid 'fibrous or filamentary materials' having either of the following characteristics:
1. A 'specific modulus' exceeding 10 × 106 m; or
2. A 'specific tensile strength' exceeding 17 × 104 m;
b. Glass 'fibrous or filamentary materials' having either of the following characteristics:
1. A 'specific modulus' exceeding 3,18 × 106 m; or
2. A 'specific tensile strength' exceeding 76,2 × 103 m;
c. Thermoset resin-impregnated continuous 'yarns', 'rovings', 'tows' or 'tapes' with a width of 15 mm or less (once prepregs), made from carbon or glass 'fibrous or filamentary materials' other than those specified in II.A1.010.a. or b.
Note: This item does not cover 'fibrous or filamentary materials' defined in items 1C010.a, 1C010.b, 1C210.a and 1C210.b. | 1C010.a
1C010.b
1C210.a
1C210.b
|
II.A1.010 | Resin-impregnated or pitch-impregnated fibres (prepregs), metal or carboncoated fibres (preforms) or 'carbon fibre preforms', as follows:
a. Made from 'fibrous or filamentary materials' specified in II.A1.009 above;
b. Epoxy resin 'matrix' impregnated carbon 'fibrous or filamentary materials' (prepregs), specified in 1C010.a, 1C010.b or 1C010.c, for the repair of aircraft structures or laminates, of which the size of individual sheets does not exceed 50 cm × 90 cm;
c. Prepregs specified in 1C010.a, 1C010.b or 1C010.c, when impregnated with phenolic or epoxy resins having a glass transition temperature (Tg) less than 433 K (160 °C) and a cure temperature lower than the glass transition temperature.
Note: This item does not cover 'fibrous or filamentary materials' defined in item 1C010.e. | 1C010.e.
1C210
|
II.A1.011 | Reinforced silicon carbide ceramic composites usable for nose tips, re-entry vehicles, nozzle flaps, usable in 'missiles', other than those specified in 1C107. | 1C107 |
II.A1.012 | Maraging steels, other than those specified in 1C116 or 1C216, 'capable of' an ultimate tensile strength of 2 050 MPa or more, at 293 K (20 °C).
Technical Note:The phrase 'maraging steel capable of' encompasses maraging steel before or after heat treatment.
| 1C216 |
II.A1.013 | Tungsten, tantalum, tungsten carbide, tantalum carbide and alloys, having both of the following characteristics:
a. In forms having a hollow cylindrical or spherical symmetry (including cylinder segments) with an inside diameter between 50 mm and 300 mm; and
b. A mass greater than 5 kg.
Note: This item does not cover tungsten, tungsten carbide and alloys defined in item 1C226. | 1C226 |
II.A1.014 | Elemental powders of cobalt, neodymium or samarium or alloys or mixtures thereof containing at least 20 % by weight of cobalt, neodymium or samarium, with a particle size less than 200 μm. | — |
II.A1.015 | Pure tributyl phosphate (TBP) [CAS No 126-73-8] or any mixture having a TBP content of more than 5 % by weight. | — |
II.A1.016 | Maraging steel, other than those prohibited by 1C116, 1C216 or II.A1.012
Technical Note:Maraging steels are iron alloys generally characterised by high nickel, very low carbon content and the use of substitutional elements or precipitates to produce strengthening and age-hardening of the alloy.
| — |
II.A1.017 | Metals, metal powders and material as follows:
a. Tungsten and tungsten alloys, other than those prohibited by 1C117, in the form of uniform spherical or atomized particles of 500 μm diameter or less with a tungsten content of 97 % by weight or more;
b. Molybdenum and molybdenum alloys, other than those prohibited by 1C117, in the form of uniform spherical or atomized particles of 500 μm diameter or less with a molybdenum content of 97 % by weight or more;
c. Tungsten materials in the solid form, other than those prohibited by 1C226, or II.A1.013 having material compositions as follows:
1. Tungsten and alloys containing 97 % by weight or more of tungsten;
2. Copper infiltrated tungsten containing 80 % by weight or more of tungsten; or
3. Silver infiltrated tungsten containing 80 % by weight or more of tungsten.
| — |
II.A1.018 | Soft magnetic alloys having a chemical composition as follows:
(a) Iron content between 30 % and 60 %, and
(b) Cobalt content between 40 % and 60 %.
| — |
II.A1.019 | "Fibrous or filamentary materials" or prepregs, not prohibited by Annex I or by Annex II (under II.A1.009, II.A1.010) of this Regulation, or not specified by Annex I of Regulation (EC) No 428/2009, as follows:
(a) Carbon "fibrous or filamentary materials";
Note: II.A1.019a. does not cover fabrics. (b) Thermoset resin-impregnated continuous "yarns", "rovings", "tows", or "tapes", made from carbon "fibrous or filamentary materials";
(c) Polyacrylonitrile (PAN) continuous "yarns", "rovings", "tows" or "tapes"
| — |