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 %. II.A1.002 Fluorine gas CAS: [7782-41-4], with a purity of at least 95 %. II.A1.003 Ring-shaped seals and gaskets, having an inner diameter of 400 mm or less, made of any of the following materials: a. Copolymers of vinylidene fluoride having 75 % or more beta crystalline structure without stretching; b. Fluorinated polyimides containing 10 % by weight or more of combined fluorine; c. Fluorinated phosphazene elastomers containing 30 % by weight or more of combined fluorine; d. Polychlorotrifluoroethylene (PCTFE, e.g. Kel-F ®); e. Fluoro-elastomers (e.g. Viton ®, Tecnoflon ®); f. Polytetrafluoroethylene (PTFE). 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: 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). Technical note: 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. Technical note: 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: a. Aramid ‘fibrous or filamentary materials’ having either of the following characteristics: 1.A ‘specific modulus’ exceeding 10 × 10^(6) m; or 2.A ‘specific tensile strength’ exceeding 17 × 10^(4) m; b. Glass ‘fibrous or filamentary materials’ having either of the following characteristics: 1.A ‘specific modulus’ exceeding 3,18 × 10^(6) m; or 2.A ‘specific tensile strength’ exceeding 76,2 × 10^(3) m; c. 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; d. Carbon ‘fibrous or filamentary materials’; e. Thermoset resin-impregnated continuous ‘yarns’, ‘rovings’, ‘tows’, or ‘tapes’, made from carbon ‘fibrous or filamentary materials’; f. Polyacrylonitrile (PAN) continuous ‘yarns’, ‘rovings’, ‘tows’ or ‘tapes’; g. Para-aramid ‘fibrous or filamentary materials’ (Kevlar® and other Kevlar®-like fibres). 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: a. Made from ‘fibrous or filamentary materials’ specified in I.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. 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: 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. 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. 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 specified by 1C116 or 1C216. Technical notes: 1. The phrase maraging steel ‘capable of’ encompasses maraging steel before or after heat treatment. 2. 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: 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; b. 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; c. 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. 1C117 1C226 II.A1.018 Soft magnetic alloys, other than those specified in 1C003, having a chemical composition as follows: a. Iron content between 30 % and 60 %; and b. Cobalt content between 40 % and 60 %. 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: a. Steel alloys ‘capable of’ ultimate tensile strength of 1200 MPa or more, at 293 K (20 °C); or b. Nitrogen-stabilised duplex stainless steel. Note: the phrase alloys ‘capable of’ encompasses alloys before or after heat 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/cm^(3) and with a detonation speed higher than 5000 m/s. 1C239

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Source: EUR-Lex (Cellar) · retrieved 2026-11-06 · Text as adopted (Official Journal); later amendments are not incorporated in this text.