Regulation (EU) 2021/821 of the European Parliament and of the Council of 20 May 2021 setting up a Union regime for the control of exports, brokering, technical assistance, transit and transfer of dual-use items (recast)

f. Polybiphenylenethersulphone having a 'glass transition temperature (Tg)' exceeding 563 K (290 °C).

1.

For the purposes of 1C008.a.2. thermoplastic materials, 1C008.a.4. materials and 1C008.f. materials, the 'glass transition temperature (Tg)' is determined using the method described in ISO 11357-2:1999 or national equivalents

2.

For the purposes of 1C008.a.2. thermosetting materials and 1C008.a.3. materials, the 'glass transition temperature (Tg)' is determined using the 3-point bend method described in ASTM D 7028-07 or equivalent national standard. The test is to be performed using a dry test specimen which has attained a minimum of 90 % degree of cure as specified by ASTM E 2160-04 or equivalent national standard, and was cured using the combination of standard- and post-cure processes that yield the highest Tg.

1C009Unprocessed fluorinated compounds as follows:

a. Not used;

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.

1C010"Fibrous or filamentary materials", as follows:

N.B.

SEE ALSO 1C210 AND 9C110.

1.

For the purposes of calculating "specific tensile strength", "specific modulus" or specific weight of "fibrous or filamentary materials" in 1C010.a., 1C010.b., 1C010.c. or 1C010.e.1.b., the tensile strength and modulus should be determined by using Method A described in ISO 10618:2004 or national equivalents.

2.

For the purposes of assessing the "specific tensile strength", "specific modulus" or specific weight of non-unidirectional "fibrous or filamentary materials" (e.g., fabrics, random mats or braids) in 1C010, this is to be based on the mechanical properties of the constituent unidirectional monofilaments (e.g., monofilaments, yarns, rovings or tows) prior to processing into the non-unidirectional "fibrous or filamentary materials".

a. Organic "fibrous or filamentary materials", having all of the following:

Note:

1C010.a. does not control polyethylene.

b. Carbon "fibrous or filamentary materials", having all of the following:

Note:

1C010.b. does not control: a. "Fibrous or filamentary materials", 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. 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:

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

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:

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

Technical Note: For the purposes of 1C010.d.2., '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:

a. Inorganic "fibrous or filamentary materials" specified in 1C010.c.; or b. Organic or carbon "fibrous or filamentary materials", having all 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^oC) and having a phenolic resin; or c. 'Dynamic Mechanical Analysis glass transition temperature (DMA Tg)' equal to or exceeding 505 K (232^oC) 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.

For the purposes of 1C010.e. and Note 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.

For the purposes of 1C010.e.2. materials, 'Dynamic Mechanical Analysis glass transition temperature (DMA Tg)' 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.

1C011Metals 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:

For the purposes of 1C011.a., 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:

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);

e. Iodine pentafluoride (CAS 7783-66-6).

N.B.

For metal powders mixed with other substances to form a mixture formulated for military purposes, see Military Goods Controls.

1C012Materials as follows:

For the purposes of 1C012., 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.

1C101Materials 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.

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

1C102Resaturated pyrolised carbon-carbon materials designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

1C107Graphite 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:

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).

1C111Propellants and constituent chemicals for propellants, other than those specified in 1C011, as follows:

a. Propulsive substances:

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

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:

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.

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.

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);

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.

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

b. Polymeric substances:

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).

c. Other propellant additives and agents:

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.

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.

1C116Maraging 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:

b. Any of the following forms:

Maraging steels are iron alloys:

1. Generally characterised by high nickel content, carbon content of less than or equal to 0,03 % by weight, 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).

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

1C117Materials 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:

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

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.

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

1C118Titanium-stabilised duplex stainless steel (Ti-DSS) having all of the following:

a. Having all of the following characteristics:

b. Having any of the following forms:

1C202Alloys, other than those specified in 1C002.b.3. or .b.4., as follows:

a. Aluminium alloys having both of the following characteristics:

b. Titanium alloys having both of the following characteristics:

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:

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:

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".

1C216Maraging 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.

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.

1C227Calcium 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.

1C228Magnesium 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.

1C229Bismuth 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.

1C230Beryllium 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.

1C231Hafnium 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.

1C232Helium-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.

1C233Lithium 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.

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

1C234Zirconium 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.

1C235Tritium, 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.

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)

1C237Radium-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.

1C238Chlorine trifluoride (ClF3).

1C239High 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.

1C240Nickel powder and porous nickel metal, other than those specified in 0C005, as follows:

a. Nickel powder having both of the following characteristics:

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.

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.

1C241Rhenium, 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.

1C350Chemicals, 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.

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

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

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

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, .89 and .90 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.

1C351Human 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:

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:

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:

12 Clostridium perfringens epsilon toxin producing types;

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).

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

Note:

1C351.d. does not control botulinum neurotoxins 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:

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:

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

b. Not used.

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".

1C354Plant 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:

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:

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:

1C450Toxic 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:

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:

Note:

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

N.B.

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

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);

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.

1C513'High-entropy alloy' or ‘refractory metal and alloy’ powders, not specified in 1C002, having a surface modified with 'inoculants'.

For the purposes of 1C513.:

1. 'High-entropy alloys' are alloys having at least 5 principal metallic elements, each having concentration within the range of 5 to 35 atomic percent, from the following list: Al, Ti, V, Cr, Mn, Fe, Co, Ni, Cu, Zr, Nb, Mo, Hf, Ta or W.

2. 'Inoculants' are additives that promote grain nucleation and increase the total area of grain boundaries to inhibit solidification defects.

3. 'Refractory metals and alloys' include the following metals and their alloys: niobium, molybdenum, tungsten and tantalum.

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.

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.

1E002Other "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:

a. Any of the following compositions:

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

c. Being any of the following:

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

N.B.

For quiet running bearings, see the Military Goods Controls.

2A001Anti-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: For the purposes of 2A001.a.: 1.

'Ring' is a annular part of a radial rolling bearing incorporating one or more raceways (ISO 5593:1997). 2.

'Rolling element' is a 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:

2A101Radial 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.

2A225Crucibles made of materials resistant to liquid actinide metals, as follows:

a. Crucibles having both of the following characteristics:

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:

c. Crucibles having all of the following characteristics:

2A226Valves 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.

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

1.

For the purposes of 2B, 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°. 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.

For the purposes of 2B, axis nomenclature shall be in accordance with 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.

For the purposes of 2B, '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" (

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

x,

y, …);

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.