Commission Delegated Regulation (EU) 2023/66 of 21 October 2022 amending Regulation (EU) 2021/821 of the European Parliament and of the Council as regards the list of dual-use items

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

• c. Inorganic "fibrous or filamentary materials", having all of the following:

• 1. Having any of the following:

• a. Composed of 50 % or more by weight silicon dioxide and having a "specific modulus" exceeding 2,54 × 10⁶ m; or

• b. Not specified in 1C010.c.1.a. and having a "specific modulus" exceeding 5,6 × 10⁶ m; and

• 1. Melting, softening, decomposition or sublimation point exceeding 1 922 K (1 649 °C) in an inert environment;

• Note: 1C010.c. does not control:

• a. Discontinuous, multiphase, polycrystalline alumina fibres in chopped fibre or random mat form, containing 3 % by weight or more silica, with a "specific modulus" of less than 10 × 10⁶ m;

• b. Molybdenum and molybdenum alloy fibres;

• c. Boron fibres;

• d. Discontinuous ceramic fibres with a melting, softening, decomposition or sublimation point lower than 2 043 K (1 770 °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 1C008.a.; or

• b. Materials specified in 1C008.d. to 1C008.f.; or

• 1. Composed of materials specified in 1C010.d.1.a. or 1C010.d.1.b. and ‘commingled’ with other fibres specified in 1C010.a., 1C010.b. or 1C010.c.;

Technical Note:

‘Commingled’ is filament to filament blending of thermoplastic fibres and reinforcement fibres in order to produce a fibre reinforcement "matrix" mix in total fibre form.

• e. Fully or partially resin-impregnated or pitch-impregnated "fibrous or filamentary materials" (prepregs), metal or carbon-coated "fibrous or filamentary materials" (preforms) or ‘carbon fibre preforms’, having all of the following:

• 1. Having any of the following:

• a. Inorganic "fibrous or filamentary materials" specified in 1C010.c.; or

• b. Organic or carbon "fibrous or filamentary materials", having all of the following:

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

• 1. "Specific tensile strength" exceeding 17,7 × 10⁴ m; and

• 1. Having any of the following:

• a. Resin or pitch, specified in 1C008 or 1C009.b.;

• b. ‘Dynamic Mechanical Analysis glass transition temperature (DMA Tg)’ equal to or exceeding 453 K (180 °C) and having a phenolic resin; or

• c. ‘Dynamic Mechanical Analysis glass transition temperature (DMA Tg)’ equal to or exceeding 505 K (232 °C) and having a resin or pitch, not specified in 1C008 or 1C009.b., and not being a phenolic resin;

• Note 1: Metal or carbon-coated "fibrous or filamentary materials" (preforms) or ‘carbon fibre preforms’, not impregnated with resin or pitch, are specified by "fibrous or filamentary materials" in 1C010.a., 1C010.b. or 1C010.c.

• Note 2: 1C010.e. does not control:

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

• 1. An area not exceeding 1 m²;

• 2. A length not exceeding 2,5 m; 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 in 1C008 or 1C009.b.

Technical Notes:

• 1. ‘Carbon fibre preforms’ are an ordered arrangement of uncoated or coated fibres intended to constitute a framework of a part before the "matrix" is introduced to form a "composite".

• 2. The ‘Dynamic Mechanical Analysis glass transition temperature (DMA Tg)’ for materials specified in 1C010.e. is determined using the method described in ASTM D 7028-07, or equivalent national standard, on a dry test specimen. In the case of thermoset materials, degree of cure of a dry test specimen shall be a minimum of 90 % as defined by ASTM E 2160-04 or equivalent national standard.

1C011 Metals and compounds, as follows:

• N.B. SEE ALSO MILITARY GOODS CONTROLS AND 1C111.

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

Technical Note:

The natural content of hafnium in the zirconium (typically 2 % to 7 %) is counted with the zirconium.

• Note: The metals or alloys specified in 1C011.a. are controlled whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium.

• 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;

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

• Note: The metals or alloys specified in 1C011.b. are controlled whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium.

• c. Guanidine nitrate (CAS 506-93-4);

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

• N.B. See also Military Goods Controls for metal powders mixed with other substances to form a mixture formulated for military purposes.

1C012 Materials as follows:

Technical Note:

These materials are typically used for nuclear heat sources.

• a. Plutonium in any form with a plutonium isotopic assay of plutonium-238 of more than 50 % by weight;

• Note: 1C012.a. does not control:

• a. Shipments with a plutonium content of 1 g or less;

• b. Shipments of 3 "effective grammes" or less when contained in a sensing component in instruments.

• b. "Previously separated" neptunium-237 in any form.

• Note: 1C012.b. does not control shipments with a neptunium-237 content of 1 g or less.

1C101 Materials and devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures, other than those specified in 1C001, usable in ‘missiles’, "missile" subsystems or unmanned aerial vehicles specified in 9A012 or 9A112.a.

• Note 1: 1C101 includes:

• a. Structural materials and coatings specially designed for reduced radar reflectivity;

• b. Coatings, including paints, specially designed for reduced or tailored reflectivity or emissivity in the microwave, infrared or ultraviolet regions of the electromagnetic spectrum.

• Note 2: 1C101 does not include coatings when specially used for the thermal control of satellites.

Technical Note:

In 1C101 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

1C102 Resaturated pyrolised carbon-carbon materials designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

1C107 Graphite and ceramic materials, other than those specified in 1C007, as follows:

• a. Fine grain graphites with a bulk density of 1,72 g/cm³ or greater, measured at 288 K (15 °C), and having a grain size of 100 μm or less, usable for rocket nozzles and re-entry vehicle nose tips, which can be machined to any of the following products:

• 1. Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater;

• 1. Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; or

• 1. Blocks having a size of 120 mm × 120 mm × 50 mm or greater;

• N.B. See also 0C004.

• b. Pyrolytic or fibrous reinforced graphites, usable for rocket nozzles and reentry vehicle nose tips usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

• N.B. See also 0C004.

• c. Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in radomes usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

• d. Bulk machinable silicon-carbide reinforced unfired ceramic, usable for nose tips usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

• e. Reinforced silicon-carbide ceramic composites, usable for nose tips, reentry vehicles and nozzle flaps usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

• f. Bulk machinable ceramic composite materials consisting of an ‘Ultra High Temperature Ceramic (UHTC)’ matrix with a melting point equal to or greater than 3 000 °C and reinforced with fibres or filaments, usable for missile components (such as nose-tips, re-entry vehicles, leading edges, jet vanes, control surfaces or rocket motor throat inserts) in "missiles", space launch vehicles specified in 9A004, sounding rockets specified in 9A104 or ‘missiles’.

• Note: 1C107.f. does not control ‘Ultra High Temperature Ceramic (UHTC) ’ materials in non-composite form.

Technical Note 1:

In 1C107.f. ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

Technical Note 2:

‘Ultra High Temperature Ceramics (UHTC)’ includes:

• 1. Titanium diboride (TiB2);

• 2. Zirconium diboride (ZrB2);

• 3. Niobium diboride (NbB2);

• 4. Hafnium diboride (HfB2);

• 5. Tantalum diboride (TaB2);

• 6. Titanium carbide (TiC);

• 7. Zirconium carbide (ZrC);

• 8. Niobium carbide (NbC);

• 9. Hafnium carbide (HfC);

• 10. Tantalum carbide (TaC).

1C111 Propellants and constituent chemicals for propellants, other than those specified in 1C011, as follows:

• a. Propulsive substances:

• 1. Spherical or spheroidal aluminium powder other than that specified in the Military Goods Controls, in particle size of less than 200 μm and an aluminium content of 97 % by weight or more, if at least 10 % of the total weight is made up of particles of less than 63 μm, according to ISO 2591-1:1988 or national equivalents;

Technical Note:

A particle size of 63 μm (ISO R-565) corresponds to 250 mesh (Tyler) or 230 mesh (ASTM standard E-11).

• 1. Metal powders, other than that specified in the Military Goods Controls, as follows:

• a. Metal powders of zirconium, beryllium or magnesium, or alloys of these metals, if at least 90 % of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spheroidal, flaked or ground, consisting 97 % by weight or more of any of the following:

• 1. Zirconium;

• 1. Beryllium; or

• 1. Magnesium;

Technical Note:

The natural content of hafnium in the zirconium (typically 2 % to 7 %) is counted with the zirconium.

• b. Metal powders of either boron or boron alloys with a boron content of 85 % or more by weight, if at least 90 % of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spheroidal, flaked or ground;

• Note: 1C111a.2.a. and 1C111a.2.b. controls powder mixtures with a multimodal particle distribution (e.g. mixtures of different grain sizes) if one or more modes are controlled.

• 1. Oxidiser substances usable in liquid propellant rocket engines as follows:

• a. Dinitrogen trioxide (CAS 10544-73-7);

• b. Nitrogen dioxide (CAS 10102-44-0)/dinitrogen tetroxide (CAS 10544-72-6);

• c. Dinitrogen pentoxide (CAS 10102-03-1);

• d. Mixed Oxides of Nitrogen (MON);

Technical Note:

Mixed Oxides of Nitrogen (MON) are solutions of Nitric Oxide (NO) in Dinitrogen Tetroxide/Nitrogen Dioxide (N2O4/NO2 ) that can be used in missile systems. There are a range of compositions that can be denoted as MONi or MONij, where i and j are integers representing the percentage of Nitric Oxide in the mixture (e.g., MON3 contains 3 % Nitric Oxide, MON25 25 % Nitric Oxide. An upper limit is MON40, 40 % by weight).

• e. SEE MILITARY GOODS CONTROLS FOR Inhibited Red Fuming Nitric Acid (IRFNA);

• f. SEE MILITARY GOODS CONTROLS AND 1C238 FOR compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen.

• 1. Hydrazine derivatives as follows:

• N.B. SEE ALSO MILITARY GOODS CONTROLS.

• a. Trimethylhydrazine (CAS 1741-01-1);

• b. Tetramethylhydrazine (CAS 6415-12-9);

• c. N,N-Diallylhydrazine (CAS 5164-11-4);

• d. Allylhydrazine (CAS 7422-78-8);

• e. Ethylene dihydrazine (CAS 6068-98-0);

• f. Monomethylhydrazine dinitrate;

• g. Unsymmetrical dimethylhydrazine nitrate;

• h. Hydrazinium azide (CAS 14546-44-2);

• i. 1,1-Dimethylhydrazinium azide (CAS 227955-52-4) / 1,2-Dimethylhydrazinium azide (CAS 299177-50-7);

• j. Hydrazinium dinitrate (CAS 13464-98-7);

• k. Diimido oxalic acid dihydrazine (CAS 3457-37-2);

• l. 2-hydroxyethylhydrazine nitrate (HEHN);

• m. See Military Goods Controls for Hydrazinium perchlorate;

• n. Hydrazinium diperchlorate (CAS 13812-39-0);

• o. Methylhydrazine nitrate (MHN) (CAS 29674-96-2);

• p. 1,1-Diethylhydrazine nitrate (DEHN) / 1,2-Diethylhydrazine nitrate (DEHN) (CAS 363453-17-2);

• q. 3,6-Dihydrazino tetrazine nitrate (1,4-dihydrazine nitrate) (DHTN);

• 1. High energy density materials, other than that specified in the Military Goods Controls, usable in ‘missiles’ or unmanned aerial vehicles specified in 9A012 or 9A112.a.;

• a. Mixed fuel that incorporate both solid and liquid fuels, such as boron slurry, having a mass-based energy density of 40 × 10⁶ J/kg or greater;

• b. Other high energy density fuels and fuel additives (e.g., cubane, ionic solutions, JP-10) having a volume-based energy density of 37,5 × 10⁹ J/m³ or greater, measured at 20 °C and one atmosphere (101,325 kPa) pressure;

• Note: 1C111.a.5.b. does not control fossil refined fuels and biofuels produced from vegetables, including fuels for engines certified for use in civil aviation, unless specially formulated for ‘missiles’ or unmanned aerial vehicles specified in 9A012 or 9A112.a..

Technical Note:

In 1C111.a.5. ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

• 1. Hydrazine replacement fuels as follows:

• a. 2-Dimethylaminoethylazide (DMAZ) (CAS 86147-04-8);

• b. Polymeric substances:

• 1. Carboxy-terminated polybutadiene (including carboxyl-terminated polybutadiene) (CTPB);

• 1. Hydroxy-terminated polybutadiene (including hydroxyl-terminated polybutadiene) (HTPB) (CAS 69102-90-5), other than that specified in the Military Goods Controls;

• 1. Polybutadiene-acrylic acid (PBAA);

• 1. Polybutadiene-acrylic acid-acrylonitrile (PBAN) (CAS 25265-19-4 / CAS 68891-50-9);

• 1. Polytetrahydrofuran polyethylene glycol (TPEG);

Technical Note:

Polytetrahydrofuran polyethylene glycol (TPEG) is a block co-polymer of poly 1,4-Butanediol (CAS 110-63-4) and polyethylene glycol (PEG) (CAS 25322-68-3).

• 1. SEE MILITARY GOODS CONTROLS FOR polyglycidyl nitrate (PGN or poly-GLYN) (CAS 27814-48-8).

• c. Other propellant additives and agents:

• 1. SEE MILITARY GOODS CONTROLS FOR Carboranes, decaboranes, pentaboranes and derivatives thereof;

• 1. Triethylene glycol dinitrate (TEGDN) (CAS 111-22-8);

• 1. 2-Nitrodiphenylamine (CAS 119-75-5);

• 1. SEE MILITARY GOODS CONTROLS FOR trimethylolethane trinitrate (TMETN) (CAS 3032-55-1);

• 1. Diethylene glycol dinitrate (DEGDN) (CAS 693-21-0);

• 1. Ferrocene derivatives as follows:

• a. SEE MILITARY GOODS CONTROLS FOR catocene (CAS 37206-42-1);

• b. SEE MILITARY GOODS CONTROLS FOR Ethyl ferrocene (CAS 1273-89-8);

• c. SEE MILITARY GOODS CONTROLS FOR n-Propyl ferrocene (CAS 1273-92-3)/iso-propyl ferrocene (CAS 12126-81-7);

• d. SEE MILITARY GOODS CONTROLS FOR n-butyl ferrocene (CAS 31904-29-7);

• e. SEE MILITARY GOODS CONTROLS FOR Pentyl ferrocene (CAS 1274-00-6);

• f. SEE MILITARY GOODS CONTROLS FOR Dicyclopentyl ferrocene (CAS 125861-17-8);

• g. SEE MILITARY GOODS CONTROLS FOR Dicyclohexyl ferrocene;

• h. SEE MILITARY GOODS CONTROLS FOR Diethyl ferrocene (CAS 1273-97-8);

• i. SEE MILITARY GOODS CONTROLS FOR Dipropyl ferrocene;

• j. SEE MILITARY GOODS CONTROLS FOR Dibutyl ferrocene (CAS 1274-08-4);

• k. SEE MILITARY GOODS CONTROLS FOR Dihexyl ferrocene (CAS 93894-59-8);

• l. SEE MILITARY GOODS CONTROLS FOR Acetyl ferrocene (CAS 1271-55-2) / 1,1'-diacetyl ferrocene (CAS 1273-94-5);

• m. SEE MILITARY GOODS CONTROLS FOR Ferrocene carboxylic acid (CAS 1271-42-7) / 1,1'-Ferrocenedicarboxylic acid (CAS 1293-87-4);

• n. SEE MILITARY GOODS CONTROLS FOR butacene (CAS 125856-62-4);

• o. Other ferrocene derivatives usable as rocket propellant burning rate modifiers, other than those specified in the Military Goods Controls.

• Note: 1C111.c.6.o. does not control ferrocene derivatives that contain a six carbon aromatic functional group attached to the ferrocene molecule.

• 1. 4,5-Diazidomethyl-2-methyl-1,2,3-triazole (iso-DAMTR), other than that specified in the Military Goods Controls.

• d. ‘Gel propellants’, other than that specified in the Military Goods Controls, specifically formulated for use in ‘missiles’.

Technical Notes:

• 1. In 1C111.d. a ‘gel propellant’ is a fuel or oxidiser formulation using a gellant such as silicates, kaolin (clay), carbon or any polymeric gellant.

• 2. In 1C111.d. a ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

• Note: For propellants and constituent chemicals for propellants not specified in 1C111, see the Military Goods Controls.

1C116 Maraging steels, useable in ‘missiles’, having all of the following:

• N.B. SEE ALSO 1C216.

• a. Having an ultimate tensile strength, measured at 293 K (20 °C), equal to or greater than:

• 1. 0,9 GPa in the solution annealed stage; or

• 1. 1,5 GPa in the precipitation hardened stage; and

• b. Any of the following forms:

• 1. Sheet, plate or tubing with a wall or plate thickness equal to or less than 5,0 mm;

• 1. Tubular forms with a wall thickness equal to or less than 50 mm and having an inner diameter equal to or greater than 270 mm.

Technical Note 1:

Maraging steels are iron alloy:

• 1. 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; and

• 2. Subjected to heat treatment cycles to facilitate the martensitic transformation process (solution annealed stage) and subsequently age hardened (precipitation hardened stage).

Technical Note 2:

In 1C116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

1C117 Materials for the fabrication of ‘missiles’ components as follows:

• a. Tungsten and alloys in particulate form with a tungsten content of 97 % by weight or more and a particle size of 50 × 10^-6 m (50 μm) or less;

• b. Molybdenum and alloys in particulate form with a molybdenum content of 97 % by weight or more and a particle size of 50 × 10^-6 m (50 μm) or less;

• c. Tungsten materials in solid form having all of the following:

• 1. Any of the following material compositions:

• a. Tungsten and alloys containing 97 % by weight or more of tungsten;

• b. Copper infiltrated tungsten containing 80 % by weight or more of tungsten; or

• c. Silver infiltrated tungsten containing 80 % by weight or more of tungsten; and

• 1. Able to be machined to any of the following products:

• a. Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater;

• b. Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; or

• c. Blocks having a size of 120 mm by 120 mm by 50 mm or greater.

Technical Note:

In 1C117 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

1C118 Titanium-stabilised duplex stainless steel (Ti-DSS) having all of the following:

• a. Having all of the following characteristics:

• 1. Containing 17,0 - 23,0 % by weight of chromium and 4,5 - 7,0 % by weight of nickel;

• 1. Having a titanium content of greater than 0,10 % by weight; and

• 1. A ferritic-austenitic microstructure (also referred to as a two-phase microstructure) of which at least 10 % by volume (according to ASTM E-1181-87 or national equivalents) is austenite; and

• b. Having any of the following forms:

• 1. Ingots or bars having a size of 100 mm or more in each dimension;

• 1. Sheets having a width of 600 mm or more and a thickness of 3 mm or less; or

• 1. Tubes having an outer diameter of 600 mm or more and a wall thickness of 3 mm or less.

1C202 Alloys, other than those specified in 1C002.b.3. or .b.4., as follows:

• a. Aluminium alloys having both of the following characteristics:

• 1. ‘Capable of’ an ultimate tensile strength of 460 MPa or more at 293 K (20 °C); and

• 1. In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm;

• b. Titanium alloys having both of the following characteristics:

• 1. ‘Capable of’ an ultimate tensile strength of 900 MPa or more at 293 K (20 °C); and

• 1. In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm.

Technical Note:

The phrase alloys ‘capable of’ encompasses alloys before or after heat treatment.

1C210

‘Fibrous or filamentary materials’ or prepregs, other than those specified in 1C010.a., .b. or .e., as follows:

• a. Carbon or aramid ‘fibrous or filamentary materials’ having either of the following characteristics:

• 1. A "specific modulus" of 12,7 × 10⁶ m or greater; or

• 1. A "specific tensile strength" of 23,5 × 10⁴ m or greater;

• Note: 1C210.a. does not control aramid ‘fibrous or filamentary materials’ having 0,25 % by weight or more of an ester based fibre surface modifier;

• b. Glass ‘fibrous or filamentary materials’ having both of the following characteristics:

• 1. A "specific modulus" of 3,18 × 10⁶ m or greater; and

• 1. A "specific tensile strength" of 7,62 × 10⁴ m or greater;

• c. Thermoset resin impregnated continuous "yarns", "rovings", "tows" or "tapes" with a width of 15 mm or less (prepregs), made from carbon or glass ‘fibrous or filamentary materials’ specified in 1C210.a. or .b.

Technical Note:

The resin forms the matrix of the composite.

• Note: In 1C210, ‘fibrous or filamentary materials’ is restricted to continuous "monofilaments", "yarns", "rovings", "tows" or "tapes".

1C216 Maraging steel, other than that specified in 1C116, ‘capable of’ an ultimate tensile strength of 1 950 MPa or more, at 293 K (20 °C).

• Note: 1C216 does not control forms in which all linear dimensions are 75 mm or less.

Technical Note:

The phrase maraging steel ‘capable of’ encompasses maraging steel before or after heat treatment.

1C225 Boron enriched in the boron-10 (¹⁰B) isotope to greater than its natural isotopic abundance, as follows: elemental boron, compounds, mixtures containing boron, manufactures thereof, waste or scrap of any of the foregoing.

• Note: In 1C225 mixtures containing boron include boron loaded materials.

Technical Note:

The natural isotopic abundance of boron-10 is approximately 18,5 weight per cent (20 atom per cent).

1C226 Tungsten, tungsten carbide, and alloys containing more than 90 % tungsten by weight, other than that specified in 1C117, having both of the following characteristics:

• a. In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 mm and 300 mm; and

• b. A mass greater than 20 kg.

• Note: 1C226 does not control manufactures specially designed as weights or gamma-ray collimators.

1C227 Calcium having both of the following characteristics:

• a. Containing less than 1 000 ppm by weight of metallic impurities other than magnesium; and

• b. Containing less than 10 ppm by weight of boron.

1C228 Magnesium having both of the following characteristics:

• a. Containing less than 200 ppm by weight of metallic impurities other than calcium; and

• b. Containing less than 10 ppm by weight of boron.

1C229 Bismuth having both of the following characteristics:

• a. A purity of 99,99 % or greater by weight; and

• b. Containing less than 10 ppm by weight of silver.

1C230 Beryllium metal, alloys containing more than 50 % beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing, other than that specified in the Military Goods Controls.

• N.B. SEE ALSO MILITARY GOODS CONTROLS.

• Note: 1C230 does not control the following:

• a. Metal windows for X-ray machines, or for bore-hole logging devices;

• b. Oxide shapes in fabricated or semi-fabricated forms specially designed for electronic component parts or as substrates for electronic circuits;

• c. Beryl (silicate of beryllium and aluminium) in the form of emeralds or aquamarines.

1C231 Hafnium metal, alloys containing more than 60 % hafnium by weight, hafnium compounds containing more than 60 % hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing.

1C232 Helium-3 (³He), mixtures containing helium-3, and products or devices containing any of the foregoing.

• Note: 1C232 does not control a product or device containing less than 1 g of helium-3.

1C233 Lithium enriched in the lithium-6 (⁶Li) isotope to greater than its natural isotopic abundance, and products or devices containing enriched lithium, as follows: elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.

• Note: 1C233 does not control thermoluminescent dosimeters.

Technical Note:

The natural isotopic abundance of lithium-6 is approximately 6,5 weight per cent (7,5 atom per cent).

1C234 Zirconium with a hafnium content of less than 1 part hafnium to 500 parts zirconium by weight, as follows: metal, alloys containing more than 50 % zirconium by weight, compounds, manufactures thereof, waste or scrap of any of the foregoing, other than those specified in 0A001.f.

• Note: 1C234 does not control zirconium in the form of foil having a thickness of 0,10 mm or less.

1C235 Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1 000, and products or devices containing any of the foregoing.

• Note: 1C235 does not control a product or device containing less than 1,48 × 10³ GBq (40 Ci) of tritium.

1C236

‘Radionuclides’ appropriate for making neutron sources based on alpha-n reaction, other than those specified in 0C001 and 1C012.a., in the following forms:

• a. Elemental;

• b. Compounds having a total activity of 37 GBq/kg (1 Ci/kg) or greater;

• c. Mixtures having a total activity of 37 GBq/kg (1 Ci/kg) or greater;

• d. Products or devices containing any of the foregoing.

• Note: 1C236 does not control a product or device containing less than 3,7 GBq (100 millicuries) of activity.

Technical Note:

In 1C236 ‘radionuclides’ are any of the following:

• — Actinium-225 (²²⁵Ac)

• — Actinium-227 (²²⁷Ac)

• — Californium-253 (²⁵³Cf)

• — Curium-240 (²⁴⁰Cm)

• — Curium-241 (²⁴¹Cm)

• — Curium-242 (²⁴²Cm)

• — Curium-243 (²⁴³Cm)

• — Curium-244 (²⁴⁴Cm)

• — Einsteinium-253 (²⁵³Es)

• — Einsteinium-254 (²⁵⁴Es)

• — Gadolinium-148 (¹⁴⁸Gd)

• — Plutonium-236 (²³⁶Pu)

• — Plutonium-238 (²³⁸Pu)

• — Polonium-208 ( ²⁰⁸Po)

• — Polonium-209 (²⁰⁹Po)

• — Polonium-210 (²¹⁰Po)

• — Radium-223 (²²³Ra)

• — Thorium-227 (²²⁷Th)

• — Thorium-228 (²²⁸Th)

• — Uranium-230 (²³⁰U)

• — Uranium-232 (²³²U)

1C237 Radium-226 (²²⁶Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium-226, manufactures thereof, and products or devices containing any of the foregoing.

• Note: 1C237 does not control the following:

• a. Medical applicators;

• b. A product or device containing less than 0,37 GBq (10 millicuries) of radium-226.

1C238 Chlorine trifluoride (ClF3).

1C239 High explosives, other than those specified in the Military Goods Controls, or substances or mixtures containing more than 2 % by weight thereof, with a crystal density greater than 1,8 g/cm³ and having a detonation velocity greater than 8 000 m/s.

1C240 Nickel powder and porous nickel metal, other than those specified in 0C005, as follows:

• a. Nickel powder having both of the following characteristics:

• 1. A nickel purity content of 99,0 % or greater by weight; and

• 1. A mean particle size of less than 10 μm measured by American Society for Testing and Materials (ASTM) B330 standard;

• b. Porous nickel metal produced from materials specified in 1C240.a.

• Note: 1C240 does not control the following:

• a. Filamentary nickel powders;

• b. Single porous nickel sheets with an area of 1 000 cm² per sheet or less.

Technical Note:

1C240.b. refers to porous metal formed by compacting and sintering the materials in 1C240.a. to form a metal material with fine pores interconnected throughout the structure.

1C241 Rhenium, and alloys containing 90 % by weight or more rhenium; and alloys of rhenium and tungsten containing 90 % by weight or more of any combination of rhenium and tungsten, other than those specified in 1C226, having both of the following characteristics:

• a. In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 and 300 mm; and

• b. A mass greater than 20 kg.

1C350 Chemicals, which may be used as precursors for toxic chemical agents, as follows, and "chemical mixtures" containing one or more thereof:

• N.B. SEE ALSO MILITARY GOODS CONTROLS AND 1C450.

• 1. Thiodiglycol (CAS 111-48-8);

• 1. Phosphorus oxychloride (CAS 10025-87-3);

• 1. Dimethyl methylphosphonate (CAS 756-79-6);

• 1. SEE MILITARY GOODS CONTROLS for Methyl phosphonyl difluoride (CAS 676-99-3);

• 1. Methyl phosphonyl dichloride (CAS 676-97-1);

• 1. Dimethyl phosphite (DMP) (CAS 868-85-9);

• 1. Phosphorus trichloride (CAS 7719-12-2);

• 1. Trimethyl phosphite (TMP) (CAS 121-45-9);

• 1. Thionyl chloride (CAS 7719-09-7);

• 1. 3-Hydroxy-1-methylpiperidine (CAS 3554-74-3);

• 1. N,N-Diisopropyl-(beta)-aminoethyl chloride (CAS 96-79-7);

• 1. N,N-Diisopropyl-(beta)-aminoethane thiol (CAS 5842-07-9);

• 1. 3-Quinuclidinol (CAS 1619-34-7);

• 1. Potassium fluoride (CAS 7789-23-3);

• 1. 2-Chloroethanol (CAS 107-07-3);

• 1. Dimethylamine (CAS 124-40-3);

• 1. Diethyl ethylphosphonate (CAS 78-38-6);

• 1. Diethyl N,N-dimethylphosphoramidate (CAS 2404-03-7);

• 1. Diethyl phosphite (CAS 762-04-9);

• 1. Dimethylamine hydrochloride (CAS 506-59-2);

• 1. Ethyl phosphinyl dichloride (CAS 1498-40-4);

• 1. Ethyl phosphonyl dichloride (CAS 1066-50-8);

• 1. SEE MILITARY GOODS CONTROLS for Ethyl phosphonyl difluoride (CAS 753-98-0);

• 1. Hydrogen fluoride (CAS 7664-39-3);

• 1. Methyl benzilate (CAS 76-89-1);

• 1. Methyl phosphinyl dichloride (CAS 676-83-5);

• 1. N,N-Diisopropyl-(beta)-amino ethanol (CAS 96-80-0);

• 1. Pinacolyl alcohol (CAS 464-07-3);

• 1. SEE MILITARY GOODS CONTROLS for O-Ethyl O-2-diisopropylaminoethyl methylphosphonite (QL) (CAS 57856-11-8);

• 1. Triethyl phosphite (CAS 122-52-1);

• 1. Arsenic trichloride (CAS 7784-34-1);

• 1. Benzilic acid (CAS 76-93-7);

• 1. Diethyl methylphosphonite (CAS 15715-41-0);

• 1. Dimethyl ethylphosphonate (CAS 6163-75-3);

• 1. Ethyl phosphinyl difluoride (CAS 430-78-4);

• 1. Methyl phosphinyl difluoride (CAS 753-59-3);

• 1. 3-Quinuclidone (CAS 3731-38-2);

• 1. Phosphorus pentachloride (CAS 10026-13-8);

• 1. Pinacolone (CAS 75-97-8);

• 1. Potassium cyanide (CAS 151-50-8);

• 1. Potassium bifluoride (CAS 7789-29-9);

• 1. Ammonium hydrogen fluoride or ammonium bifluoride (CAS 1341-49-7);

• 1. Sodium fluoride (CAS 7681-49-4);

• 1. Sodium bifluoride (CAS 1333-83-1);

• 1. Sodium cyanide (CAS 143-33-9);

• 1. Triethanolamine (CAS 102-71-6);

• 1. Phosphorus pentasulphide (CAS 1314-80-3);

• 1. Di-isopropylamine (CAS 108-18-9);

• 1. Diethylaminoethanol (CAS 100-37-8);

• 1. Sodium sulphide (CAS 1313-82-2);

• 1. Sulphur monochloride (CAS 10025-67-9);

• 1. Sulphur dichloride (CAS 10545-99-0);

• 1. Triethanolamine hydrochloride (CAS 637-39-8);

• 1. N,N-Diisopropyl-(beta)-aminoethyl chloride hydrochloride (CAS 4261-68-1);

• 1. Methylphosphonic acid (CAS 993-13-5);

• 1. Diethyl methylphosphonate (CAS 683-08-9);

• 1. N,N-Dimethylaminophosphoryl dichloride (CAS 677-43-0);

• 1. Triisopropyl phosphite (CAS 116-17-6);

• 1. Ethyldiethanolamine (CAS 139-87-7);

• 1. O,O-Diethyl phosphorothioate (CAS 2465-65-8);

• 1. O,O-Diethyl phosphorodithioate (CAS 298-06-6);

• 1. Sodium hexafluorosilicate (CAS 16893-85-9);

• 1. Methylphosphonothioic dichloride (CAS 676-98-2);

• 1. Diethylamine (CAS 109-89-7);

• 1. N,N-Diisopropylaminoethanethiol hydrochloride (CAS 41480-75-5);

• 1. Methyl dichlorophosphate (CAS 677-24-7);

• 1. Ethyl dichlorophosphate (CAS 1498-51-7);

• 1. Methyl difluorophosphate (CAS 22382-13-4);

• 1. Ethyl difluorophosphate (CAS 460-52-6);

• 1. Diethyl chlorophosphite (CAS 589-57-1);

• 1. Methyl chlorofluorophosphate (CAS 754-01-8);

• 1. Ethyl chlorofluorophosphate (CAS 762-77-6);

• 1. N,N-Dimethylformamidine (CAS 44205-42-7);

• 1. N,N-Diethylformamidine (CAS 90324-67-7);

• 1. N,N-Dipropylformamidine (CAS 48044-20-8);

• 1. N,N-Diisopropylformamidine (CAS 857522-08-8);

• 1. N,N-Dimethylacetamidine (CAS 2909-14-0);

• 1. N,N-Diethylacetamidine (CAS 14277-06-6);

• 1. N,N-Dipropylacetamidine (CAS 1339586-99-0);

• 1. N,N-Dimethylpropanamidine (CAS 56776-14-8);

• 1. N,N-Diethylpropanamidine (CAS 84764-73-8);

• 1. N,N-Dipropylpropanamidine (CAS 1341496-89-6);

• 1. N,N-Dimethylbutanamidine (CAS 1340437-35-5);

• 1. N,N-Diethylbutanamidine (CAS 53510-30-8);

• 1. N,N-Dipropylbutanamidine (CAS 1342422-35-8);

• 1. N,N-Diisopropylbutanamidine (CAS 1315467-17-4);

• 1. N,N-Dimethylisobutanamidine (CAS 321881-25-8);

• 1. N,N-Diethylisobutanamidine (CAS 1342789-47-2);

• 1. N,N-Dipropylisobutanamidine (CAS 1342700-45-1).

• Note 1: For exports to "States not Party to the Chemical Weapons Convention", 1C350 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C350.1, .3, .5, .11, .12, .13, .17, .18, .21, .22, .26, .27, .28, .31, .32, .33, .34, .35, .36, .54, .55, .56, .57, .63 and .65 in which no individually specified chemical constitutes more than 10 % by the weight of the mixture.

• Note 2: For exports to "States Party to the Chemical Weapons Convention", 1C350 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C350.1, .3, .5, .11, .12, .13, .17, .18, .21, .22, .26, .27, .28, .31, .32, .33, .34, .35, .36, .54, .55, .56, .57, .63 and .65 in which no individually specified chemical constitutes more than 30 % by the weight of the mixture.

• Note 3: 1C350 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C350.2, .6, .7, .8, .9, .10, .14, .15, .16, .19, .20, .24, .25, .30, .37, .38, .39, .40, .41, .42, .43, .44, .45, .46, .47, .48, .49, .50, .51, .52, .53, .58, .59, .60, .61, .62, .64, .66, .67, .68, .69, .70, .71, .72, .73, .74, .75, .76, .77, .78, .79, .80, .81, .82, .83, .84, .85, .86, .87, .88 and .89 in which no individually specified chemical constitutes more than 30 % by the weight of the mixture.

• Note 4: 1C350 does not control products identified as consumer goods packaged for retail sale for personal use or packaged for individual use.

1C351 Human and animal pathogens and "toxins", as follows:

• a. Viruses, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

• 1. African horse sickness virus;

• 1. African swine fever virus;

• 1. Andes virus;

• 1. Avian influenza virus, which are:

• a. Uncharacterised; or

• b. Defined in Annex I(2) EC Directive 2005/94/EC (OJ L 10, 14.1.2006 p. 16) as having high pathogenicity, as follows:

• 1. Type A viruses with an IVPI (intravenous pathogenicity index) in 6 week old chickens of greater than 1,2; or

• 1. Type A viruses of the subtypes H5 or H7 with genome sequences codified for multiple basic amino acids at the cleavage site of the haemagglutinin molecule similar to that observed for other HPAI viruses, indicating that the haemagglutinin molecule can be cleaved by a host ubiquitous protease;

• 1. Bluetongue virus;

• 1. Chapare virus;

• 1. Chikungunya virus;

• 1. Choclo virus;

• 1. Crimean-Congo hemorrhagic fever virus;

• 1. Not used;

• 1. Dobrava-Belgrade virus;

• 1. Eastern equine encephalitis virus;

• 1. Ebolavirus: all members of the Ebolavirus genus;

• 1. Foot-and-mouth disease virus;

• 1. Goatpox virus;

• 1. Guanarito virus;

• 1. Hantaan virus;

• 1. Hendra virus (Equine morbillivirus);

• 1. Suid herpesvirus 1 (Pseudorabies virus; Aujeszky's disease);

• 1. Classical swine fever virus (Hog cholera virus);

• 1. Japanese encephalitis virus;

• 1. Junin virus;

• 1. Kyasanur Forest disease virus;

• 1. Laguna Negra virus;

• 1. Lassa virus;

• 1. Louping ill virus;

• 1. Lujo virus;

• 1. Lumpy skin disease virus;

• 1. Lymphocytic choriomeningitis virus;

• 1. Machupo virus;

• 1. Marburgvirus: all members of the Marburgvirus genus;

• 1. Monkeypox virus;

• 1. Murray Valley encephalitis virus;

• 1. Newcastle disease virus;

• 1. Nipah virus;

• 1. Omsk hemorrhagic fever virus;

• 1. Oropouche virus;

• 1. Peste-des-petits-ruminants virus;

• 1. Swine vesicular disease virus;

• 1. Powassan virus;

• 1. Rabies virus and all other members of the Lyssavirus genus;

• 1. Rift Valley fever virus;

• 1. Rinderpest virus;

• 1. Rocio virus;

• 1. Sabia virus;

• 1. Seoul virus;

• 1. Sheeppox virus;

• 1. Sin Nombre virus;

• 1. St. Louis encephalitis virus;

• 1. Porcine Teschovirus;

• 1. Tick-borne encephalitis virus (Far Eastern subtype);

• 1. Variola virus;

• 1. Venezuelan equine encephalitis virus;

• 1. Vesicular stomatitis virus;

• 1. Western equine encephalitis virus;

• 1. Yellow fever virus;

• 1. Severe acute respiratory syndrome-related coronavirus (SARS-related coronavirus);

• 1. Reconstructed 1918 influenza virus;

• 1. Middle East respiratory syndrome-related coronavirus (MERS-related coronavirus);

• b. Not used;

• c. Bacteria, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

• 1. Bacillus anthracis;

• 1. Brucella abortus;

• 1. Brucella melitensis;

• 1. Brucella suis;

• 1. Burkholderia mallei (Pseudomonas mallei);

• 1. Burkholderia pseudomallei (Pseudomonas pseudomallei);

• 1. Chlamydia psittaci (Chlamydophila psittaci);

• 1. Clostridium argentinense (formerly known as Clostridium botulinum Type G), botulinum neurotoxin producing strains;

• 1. Clostridium baratii, botulinum neurotoxin producing strains;

• 1. Clostridium botulinum;

• 1. Clostridium butyricum, botulinum neurotoxin producing strains;

• 12 Clostridium perfringens epsilon toxin producing types;

• 1. Coxiella burnetii;

• 1. Francisella tularensis;

• 1. Mycoplasma capricolum subspecies capripneumoniae (strain F38);

• 1. Mycoplasma mycoides subspecies mycoides SC (small colony);

• 1. Rickettsia prowazekii;

• 1. Salmonella enterica subspecies enterica serovar Typhi (Salmonella typhi);

• 1. Shiga toxin producing Escherichia coli (STEC) of serogroups O26, O45, O103, O104, O111, O121, O145, O157, and other shiga toxin producing serogroups;

• Note: Shiga toxin producing Escherichia coli (STEC) includes inter alia enterohaemorrhagic E. coli (EHEC), verotoxin producing E. coli (VTEC) or verocytotoxin producing E. coli (VTEC).

• 1. Shigella dysenteriae;

• 1. Vibrio cholerae;

• 1. Yersinia pestis;

• d. "Toxins", as follows, and "sub-unit of toxins" thereof:

• 1. Botulinum toxins;

• 1. Clostridium perfringens alpha, beta 1, beta 2, epsilon and iota toxins;

• 1. Conotoxins;

• 1. Ricin;

• 1. Saxitoxin;

• 1. Shiga toxins (shiga-like toxins, verotoxins and verocytotoxins)

• 1. Staphylococcus aureus enterotoxins, hemolysin alpha toxin, and toxic shock syndrome toxin (formerly known as Staphylococcus enterotoxin F);

• 1. Tetrodotoxin;

• 1. Not used;

• 1. Microcystins (Cyanginosins);

• 1. Aflatoxins;

• 1. Abrin;

• 1. Cholera toxin;

• 1. Diacetoxyscirpenol;

• 1. T-2 toxin;

• 1. HT-2 toxin;

• 1. Modeccin;

• 1. Volkensin;

• 1. Viscumin (Viscum Album Lectin 1);

• Note: 1C351.d. does not control botulinum toxins or conotoxins in product form meeting all of the following criteria:

• 1. Are pharmaceutical formulations designed for human administration in the treatment of medical conditions;

• 2. Are pre-packaged for distribution as medical products;

• 3. Are authorised by a state authority to be marketed as medical products.

• e. Fungi, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

• 1. Coccidioides immitis;

• 1. Coccidioides posadasii.

• Note: 1C351 does not control "vaccines" or "immunotoxins".

1C353

‘Genetic elements’ and ‘genetically-modified organisms’, as follows:

• a. Any ‘genetically-modified organism’ which contains, or ‘genetic element’ that codes for, any of the following:

• 1. Any gene or genes specific to any virus specified in 1C351.a. or 1C354.a.;

• 1. Any gene or genes specific to any bacterium specified in 1C351.c. or 1C354.b. or fungus specified in 1C351.e. or 1C354.c., and which is any of the following:

• a. In itself or through its transcribed or translated products represents a significant hazard to human, animal or plant health; or

• b. Could ‘endow or enhance pathogenicity’; or

• 1. Any "toxins" specified in 1C351.d. or "sub-units of toxins" therefor;

• b. Not used.

Technical Notes:

• 1. ‘Genetically-modified organisms’ include organisms in which the nucleic acid sequences have been created or altered by deliberate molecular manipulation.

• 2. ‘Genetic elements’ include inter alia chromosomes, genomes, plasmids, transposons, vectors and inactivated organisms containing recoverable nucleic acid fragments, whether genetically modified or unmodified, or chemically synthesised in whole or in part. For the purposes of the genetic elements control, nucleic acids from an inactivated organism, virus, or sample are considered recoverable if the inactivation and preparation of the material is intended or known to facilitate isolation, purification, amplification, detection, or identification of nucleic acids.

• 3. ‘Endow or enhance pathogenicity’ is defined as when the insertion or integration of the nucleic acid sequence or sequences is/are likely to enable or increase a recipient organism’s ability to be used to deliberately cause disease or death. This might include alterations to, inter alia: virulence, transmissibility, stability, route of infection, host range, reproducibility, ability to evade or suppress host immunity, resistance to medical countermeasures, or detectability.

• Note 1: 1C353 does not control nucleic acid sequences of shiga toxin producing Escherichia coli of serogroups O26, O45, O103, O104, O111, O121, O145, O157, and other shiga toxin producing serogroups, other than those genetic elements coding for shiga toxin, or for its subunits.

• Note 2: 1C353 does not control "vaccines".

1C354 Plant pathogens, as follows:

• a. Viruses, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

• 1. Andean potato latent virus (Potato Andean latent tymovirus);

• 1. Potato spindle tuber viroid;

• b. Bacteria, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material which has been deliberately inoculated or contaminated with such cultures, as follows:

• 1. Xanthomonas albilineans;

• 1. Xanthomonas axonopodis pv. citri (Xanthomonas campestris pv. citri A) [Xanthomonas campestris pv. citri];

• 1. Xanthomonas oryzae pv. oryzae (Pseudomonas campestris pv. oryzae);

• 1. Clavibacter michiganensis subsp. sepedonicus (Corynebacterium michiganensis subsp. sepedonicum or Corynebacterium sepedonicum);

• 1. Ralstonia solanacearum, race 3, biovar 2;

• c. Fungi, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material which has been deliberately inoculated or contaminated with such cultures, as follows:

• 1. Colletotrichum kahawae (Colletotrichum coffeanum var. virulans);

• 1. Cochliobolus miyabeanus (Helminthosporium oryzae);

• 1. Microcyclus ulei (syn. Dothidella ulei);

• 1. Puccinia graminis ssp. graminis var. graminis / Puccinia graminis ssp. graminis var. stakmanii (Puccinia graminis [syn. Puccinia graminis f. sp. tritici]);

• 1. Puccinia striiformis (syn. Puccinia glumarum);

• 1. Magnaporthe oryzae (Pyricularia oryzae);

• 1. Peronosclerospora philippinensis (Peronosclerospora sacchari);

• 1. Sclerophthora rayssiae var. zeae;

• 1. Synchytrium endobioticium;

• 1. Tilletia indica;

• 1. Thecaphora solani.

1C450 Toxic chemicals and toxic chemical precursors, as follows, and "chemical mixtures" containing one or more thereof:

• N.B. SEE ALSO ENTRY 1C350, 1C351.d. AND MILITARY GOODS CONTROLS.

• a. Toxic chemicals, as follows:

• 1. Amiton: O,O-Diethyl S-[2-(diethylamino)ethyl] phosphorothiolate (CAS 78-53-5) and corresponding alkylated or protonated salts;

• 1. PFIB: 1,1,3,3,3-Pentafluoro-2-(trifluoromethyl)-1-propene (CAS 382-21-8);

• 1. SEE MILITARY GOODS CONTROLS FOR BZ: 3-Quinuclidinyl benzilate (CAS 6581-06-2);

• 1. Phosgene: Carbonyl dichloride (CAS 75-44-5);

• 1. Cyanogen chloride (CAS 506-77-4);

• 1. Hydrogen cyanide (CAS 74-90-8);

• 1. Chloropicrin: Trichloronitromethane (CAS 76-06-2);

• Note 1: For exports to "States not Party to the Chemical Weapons Convention", 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C450.a.1. and .a.2. in which no individually specified chemical constitutes more than 1 % by the weight of the mixture.

• Note 2: For exports to "States Party to the Chemical Weapons Convention", 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C450.a.1. and .a.2. in which no individually specified chemical constitutes more than 30 % by the weight of the mixture.

• Note 3: 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C450.a.4., .a.5., .a.6. and .a.7. in which no individually specified chemical constitutes more than 30 % by the weight of the mixture.

• Note 4: 1C450 does not control products identified as consumer goods packaged for retail sale for personal use or packaged for individual use.

• b. Toxic chemical precursors, as follows:

• 1. Chemicals, other than those specified in the Military Goods Controls or in 1C350, containing a phosphorus atom to which is bonded one methyl, ethyl or propyl (normal or iso) group but not further carbon atoms;

• Note: 1C450.b.1. does not control Fonofos: O-Ethyl S-phenyl ethylphosphonothiolothionate (CAS 944-22-9);

• 1. N,N-Dialkyl [methyl, ethyl or propyl (normal or iso)] phosphoramidic dihalides, other than N,N-Dimethylaminophosphoryl dichloride;

• N.B. See 1C350.57. for N,N-Dimethylaminophosphoryl dichloride.

• 1. Dialkyl [methyl, ethyl or propyl (normal or iso)] N,N-dialkyl [methyl, ethyl or propyl (normal or iso)]-phosphoramidates, other than Diethyl-N,N-dimethylphosphoramidate which is specified in 1C350;

• 1. N,N-Dialkyl [methyl, ethyl or propyl (normal or iso)] aminoethyl-2-chlorides and corresponding protonated salts, other than N,N-Diisopropyl-(beta)-aminoethyl chloride or N,N-Diisopropyl-(beta)-aminoethyl chloride hydrochloride which are specified in 1C350;

- 5. N,N-Dialkyl [methyl, ethyl or propyl (normal or iso)] aminoethane-2-ols and corresponding protonated salts, other than N,N-Diisopropyl-(beta)-aminoethanol (CAS 96-80-0) and N,N-Diethylaminoethanol (CAS 100-37-8) which are specified in 1C350;

• Note: 1C450.b.5. does not control the following:

• a. N,N-Dimethylaminoethanol (CAS 108-01-0) and corresponding protonated salts;

• b. Protonated salts of N,N-Diethylaminoethanol (CAS 100-37-8);

• 1. N,N-Dialkyl [methyl, ethyl or propyl (normal or iso)] aminoethane-2-thiols and corresponding protonated salts, other than N,N-Diisopropyl-(beta)-aminoethane thiol (CAS 5842-07-9) and N,N-Diisopropylaminoethanethiol hydrochloride (CAS 41480-75-5) which are specified in 1C350;

• 1. See 1C350 for ethyldiethanolamine (CAS 139-87-7);

• 1. Methyldiethanolamine (CAS 105-59-9).

- Note 1: For exports to "States not Party to the Chemical Weapons Convention", 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C450.b.1., .b.2., .b.3., .b.4., .b.5. and .b.6. in which no individually specified chemical constitutes more than 10 % by the weight of the mixture.

• Note 2: For exports to "States Party to the Chemical Weapons Convention", 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C450.b.1., .b.2., .b.3., .b.4., .b.5. and .b.6. in which no individually specified chemical constitutes more than 30 % by the weight of the mixture.

• Note 3: 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entry 1C450.b.8. in which no individually specified chemical constitutes more than 30 % by the weight of the mixture.

• Note 4: 1C450 does not control products identified as consumer goods packaged for retail sale for personal use or packaged for individual use.

1D Software

1D001

"Software" specially designed or modified for the "development", "production" or "use" of equipment specified in 1B001 to 1B003.

1D002

"Software" for the "development" of organic "matrix", metal "matrix" or carbon "matrix" laminates or "composites".

1D003

"Software" specially designed or modified to enable equipment to perform the functions of equipment specified in 1A004.c. or 1A004.d.

1D101

"Software" specially designed or modified for the operation or maintenance of goods specified in 1B101, 1B102, 1B115, 1B117, 1B118 or 1B119.

1D103

"Software" specially designed for analysis of reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures.

1D201

"Software" specially designed for the "use" of goods specified in 1B201.

1E Technology

1E001

"Technology" according to the General Technology Note for the "development" or "production" of equipment or materials specified in 1A002 to 1A005, 1A006.b., 1A007, 1B or 1C.

1E002 Other "technology" as follows:

• a. "Technology" for the "development" or "production" of polybenzothiazoles or polybenzoxazoles;

• b. "Technology" for the "development" or "production" of fluoroelastomer compounds containing at least one vinylether monomer;

• c. "Technology" for the design or "production" of the following ceramic powders or non-"composite" ceramic materials:

• 1. Ceramic powders having all of the following:

• a. Any of the following compositions:

• 1. Single or complex oxides of zirconium and complex oxides of silicon or aluminium;

• 1. Single nitrides of boron (cubic crystalline forms);

• 1. Single or complex carbides of silicon or boron; or

• 1. Single or complex nitrides of silicon;

• b. Any of the following total metallic impurities (excluding intentional additions):

• 1. Less than 1 000 ppm for single oxides or carbides; or

• 1. Less than 5 000 ppm for complex compounds or single nitrides; and

- c. Being any of the following:

- 1. Zirconia (CAS 1314-23-4) with an average particle size equal to or less than 1 μm and no more than 10 % of the particles larger than 5 μm; or

- 2. Other ceramic powders with an average particle size equal to or less than 5 μm and no more than 10 % of the particles larger than 10 μm;

- 2. Non-"composite" ceramic materials composed of the materials specified in 1E002.c.1.;

• Note: 1E002.c.2. does not control "technology" for abrasives.

• d. Not used;

• e. "Technology" for the installation, maintenance or repair of materials specified in 1C001;

• f. "Technology" for the repair of "composite" structures, laminates or materials specified in 1A002 or 1C007.c.;

• Note: 1E002.f. does not control "technology" for the repair of "civil aircraft" structures using carbon "fibrous or filamentary materials" and epoxy resins, contained in "aircraft" manufacturers' manuals.

• g. "Libraries" specially designed or modified to enable equipment to perform the functions of equipment specified in 1A004.c. or 1A004.d.

1E101

"Technology" according to the General Technology Note for the "use" of goods specified in 1A102, 1B001, 1B101, 1B102, 1B115 to 1B119, 1C001, 1C101, 1C107, 1C111 to 1C118, 1D101 or 1D103.

1E102

"Technology" according to the General Technology Note for the "development" of "software" specified in 1D001, 1D101 or 1D103.

1E103

"Technology" for the regulation of temperature, pressure or atmosphere in autoclaves or hydroclaves, when used for the "production" of "composites" or partially processed "composites".

1E104

"Technology" for the "production" of pyrolytically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1 573 K (1 300 °C) to 3 173 K (2 900 °C) temperature range at pressures of 130 Pa to 20 kPa.

• Note: 1E104 includes "technology" for the composition of precursor gases, flow-rates and process control schedules and parameters.

1E201

"Technology" according to the General Technology Note for the "use" of goods specified in 1A002, 1A007, 1A202, 1A225 to 1A227, 1B201, 1B225 to 1B235, 1C002.b.3. or .b.4., 1C010.b., 1C202, 1C210, 1C216, 1C225 to 1C241 or 1D201.

1E202

"Technology" according to the General Technology Note for the "development" or "production" of goods specified in 1A007, 1A202 or 1A225 to 1A227.

1E203

"Technology" according to the General Technology Note for the "development" of "software" specified in 1D201.

PART IV

Category 2

CATEGORY 2 - MATERIALS PROCESSING

2A Systems, Equipment and Components

• N.B. For quiet running bearings, see the Military Goods Controls.

2A001 Anti-friction bearings, bearing systems and components, as follows:

• N.B. SEE ALSO 2A101.

• a. Ball bearings and solid roller bearings, having all tolerances specified by the manufacturer in accordance with ISO 492 Tolerance Class 4 or Class 2 (or national equivalents), or better, and having both ‘rings’ and ‘rolling elements’, made from monel or beryllium;

• Note: 2A001.a. does not control tapered roller bearings.

Technical Notes:

• 1. ‘Ring’ - annular part of a radial rolling bearing incorporating one or more raceways (ISO 5593:1997).

• 2. ‘Rolling element’ - ball or roller which rolls between raceways (ISO 5593:1997).

• b. Not used;

• c. Active magnetic bearing systems using any of the following, and specially designed components therefor:

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

• 1. All-electromagnetic 3D homopolar bias designs for actuators; or

• 1. High temperature (450 K (177 °C) and above) position sensors.

2A101 Radial ball bearings, other than those specified in 2A001, having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all of the following characteristics:

• a. An inner ring bore diameter between 12 mm and 50 mm;

• b. An outer ring outside diameter between 25 mm and 100 mm; and

• c. A width between 10 mm and 20 mm.

2A225 Crucibles made of materials resistant to liquid actinide metals, as follows:

- a. Crucibles having both of the following characteristics:

• 1. A volume of between 150 cm³ and 8 000 cm³; and

• 1. Made of or coated with any of the following materials, or combination of the following materials, having an overall impurity level of 2 % or less by weight:

• a. Calcium fluoride (CaF2);

• b. Calcium zirconate (metazirconate) (CaZrO3);

• c. Cerium sulphide (Ce2S3);

• d. Erbium oxide (erbia) (Er2O3);

• e. Hafnium oxide (hafnia) (HfO2);

• f. Magnesium oxide (MgO);

• g. Nitrided niobium-titanium-tungsten alloy (approximately 50 % Nb, 30 % Ti, 20 % W);

• h. Yttrium oxide (yttria) (Y2O3); or

• i. Zirconium oxide (zirconia) (ZrO2);

• b. Crucibles having both of the following characteristics:

• 1. A volume of between 50 cm³ and 2 000 cm³; and

• 1. Made of or lined with tantalum, having a purity of 99,9 % or greater by weight;

• c. Crucibles having all of the following characteristics:

• 1. A volume of between 50 cm³ and 2 000 cm³;

• 1. Made of or lined with tantalum, having a purity of 98 % or greater by weight; and

• 1. Coated with tantalum carbide, nitride, boride, or any combination thereof.

2A226 Valves having all of the following characteristics:

• a. A ‘nominal size’ of 5 mm or greater;

• b. Having a bellows seal; and

• c. Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60 % nickel by weight.

Technical Note:

For valves with different inlet and outlet diameters, the ‘nominal size’ in 2A226 refers to the smallest diameter.

2B Test, Inspection and Production Equipment

Technical Notes:

• 1. Secondary parallel contouring axes, (e.g., the w-axis on horizontal boring mills or a secondary rotary axis the centre line of which is parallel to the primary rotary axis) are not counted in the total number of contouring axes. Rotary axes need not rotate over 360^o. A rotary axis can be driven by a linear device (e.g., a screw or a rack-and-pinion).

• 2. For the purposes of 2B, the number of axes which can be co-ordinated simultaneously for "contouring control" is the number of axes along or around which, during processing of the workpiece, simultaneous and interrelated motions are performed between the workpiece and a tool. This does not include any additional axes along or around which other relative movement within the machine are performed such as:

• a. Wheel-dressing systems in grinding machines;

• b. Parallel rotary axes designed for mounting of separate workpieces;

• c. Co-linear rotary axes designed for manipulating the same workpiece by holding it in a chuck from different ends.

• 3. Axis nomenclature shall be in accordance with International Standard ISO 841:2001, Industrial automation systems and integration - Numerical control of machines - Coordinate system and motion nomenclature.

• 4. For the purposes of 2B001 to 2B009 a "tilting spindle" is counted as a rotary axis.

• 5. ‘Stated "unidirectional positioning repeatability" ’ may be used for each machine tool model as an alternative to individual machine tests and is determined as follows:

• a. Select five machines of a model to be evaluated;

• b. Measure the linear axis repeatability (R↑,R↓) according to ISO 230-2:2014 and evaluate "unidirectional positioning repeatability" for each axis of each of the five machines;

• c. Determine the arithmetic mean value of the "unidirectional positioning repeatability"-values for each axis of all five machines together. These arithmetic mean values of "unidirectional positioning repeatability" (

Image omitted; see official source

) become the stated value of each axis for the model (

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,

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, …);

• d. Since the Category 2 list refers to each linear axis there will be as many 'stated "unidirectional positioning repeatability" values as there are linear axes;

• e. If any axis of a machine model not specified in 2B001.a. to 2B001.c. has a 'stated "unidirectional positioning repeatability" equal to or less than the specified "unidirectional positioning repeatability" of each machine tool model plus 0,7 μm, the builder should be required to reaffirm the accuracy level once every eighteen months.

• 6. For the purposes of 2B001.a. to 2B001.c., measurement uncertainty for the "unidirectional positioning repeatability" of machine tools, as defined in the International Standard ISO 230-2:2014 or national equivalents, shall not be considered.

• 7. For the purpose of 2B001.a. to 2B001.c., the measurement of axes shall be made according to test procedures in 5.3.2. of ISO 230-2:2014. Tests for axes longer than 2 meters shall be made over 2 m segments. Axes longer than 4 m require multiple tests (e.g., two tests for axes longer than 4 m and up to 8 m, three tests for axes longer than 8 m and up to 12 m), each over 2 m segments and distributed in equal intervals over the axis length. Test segments are equally spaced along the full axis length, with any excess length equally divided at the beginning, in between, and at the end of the test segments. The smallest "unidirectional positioning repeatability"-value of all test segments is to be reported.

2B001 Machine tools and any combination thereof, for removing (or cutting) metals, ceramics or "composites", which, according to the manufacturer’s technical specification, can be equipped with electronic devices for "numerical control", as follows:

• N.B. SEE ALSO 2B201.

• Note 1: 2B001 does not control special purpose machine tools limited to the manufacture of gears. For such machines see 2B003.

• Note 2: 2B001 does not control special purpose machine tools limited to the manufacture of any of the following:

• a. Crankshafts or camshafts;

• b. Tools or cutters;

• c. Extruder worms;

• d. Engraved or facetted jewellery parts; or

• e. Dental prostheses.

• Note 3: A machine tool having at least two of the three turning, milling or grinding capabilities (e.g., a turning machine with milling capability), must be evaluated against each applicable entry 2B001.a., b. or c.

• Note 4: A machine tool having an additive manufacturing capability in addition to a turning, milling or grinding capability must be evaluated against each applicable entry 2B001.a., .b. or .c.

• N.B. For optical finishing machines, see 2B002.

• 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

• 1. "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;

• Note 1: 2B001.a. does not control turning machines specially designed for producing contact lenses, having all of the following:

• a. Machine controller limited to using ophthalmic based software for part programming data input; and

• b. No vacuum chucking.

• Note 2: 2B001.a. does not control bar machines (Swissturn), limited to machining only bar feed thru, if maximum bar diameter is equal to or less than 42 mm and there is no capability of mounting chucks. Machines may have drilling or milling capabilities for machining parts with diameters less than 42 mm.

• 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;

• 1. 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; or

• 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;

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

• 1. Fly cutting machines having all of the following:

• a. Spindle "run-out" and "camming" less (better) than 0,0004 mm TIR; and

• b. Angular deviation of slide movement (yaw, pitch and roll) less (better) than 2 seconds of arc, TIR over 300 mm of travel;

• c. Machine tools for grinding having any of the following:

• 1. Having all of the following:

• a. "Unidirectional positioning repeatability" equal to or less (better) than 1,1 μm along one or more linear axis; and

• b. Three or four axes which can be coordinated simultaneously for "contouring control"; or

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

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

• b. "Unidirectional positioning repeatability" equal to or less (better) than 1,4 μm along one or more linear axis with a travel length equal to or greater than 1 m and less than 4 m; or

• 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.

• Note: 2B001.c. does not control grinding machine as follows:

• a. Cylindrical external, internal, and external-internal grinding machines, having all of the following:

• 1. Limited to cylindrical grinding; and

• 2. Limited to a maximum workpiece capacity of 150 mm outside diameter or length.

• b. Machines designed specifically as jig grinders that do not have a z-axis or a w-axis, with a "unidirectional positioning repeatability" less (better) than 1,1 μm

• c. Surface grinders.

• d. Electrical discharge machines (EDM) of the non-wire type which have two or more rotary axes which can be coordinated simultaneously for "contouring control";

• e. Machine tools for removing metals, ceramics or "composites", having all of the following:

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

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

• b. Electron beam; or

• c. "Laser" beam; and

• 1. At least two rotary axes having all of the following:

• a. Can be coordinated simultaneously for "contouring control"; and

• b. A positioning "accuracy" of less (better) than 0,003^o;

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

2B002 Numerically controlled optical finishing machine tools equipped for selective material removal to produce non-spherical optical surfaces having all of the following characteristics:

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

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

• c. Four or more axes which can be coordinated simultaneously for "contouring control"; and

• d. Using any of the following processes:

• 1. Magnetorheological finishing (‘MRF’);

• 1. Electrorheological finishing (‘ERF’);

• 1. ‘Energetic particle beam finishing’;

• 1. ‘Inflatable membrane tool finishing’; or

• 1. ‘Fluid jet finishing’.

Technical Notes:

For the purposes of 2B002:

• 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.

2B003

"Numerically controlled" machine tools, specially designed for the shaving, finishing, grinding or honing of hardened (Rc=40 or more) spur, helical and double-helical gears having all of the following:

• a. A pitch diameter exceeding 1 250 mm;

• b. A face width of 15 % of pitch diameter or larger; and

• c. A finished quality of AGMA 14 or better (equivalent to ISO 1328 class 3).

2B004 Hot "isostatic presses" having all of the following, and specially designed components and accessories therefor:

• N.B. SEE ALSO 2B104 and 2B204.

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

• b. Having any of the following:

• 1. A maximum working pressure exceeding 207 MPa;

• 1. A controlled thermal environment exceeding 1 773 K (1 500 °C); or

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

Technical Note:

The inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.