Semi‑fabricated forms (whether or not coated, plated, drilled or punched):
a. Wrought or worked materials fabricated by rolling, drawing, extruding, forging, impact extruding, pressing, graining, atomising, and grinding, i.e.: angles, channels, circles, discs, dust, flakes, foils and leaf, forging, plate, powder, pressings and stampings, ribbons, rings, rods (including bare welding rods, wire rods, and rolled wire), sections, shapes, sheets, strip, pipe and tubes (including tube rounds, squares, and hollows), drawn or extruded wire;
b. Cast material produced by casting in sand, die, metal, plaster or other types of moulds, including high pressure castings, sintered forms, and forms made by powder metallurgy.
The object of the control should not be defeated by the export of non‑listed forms alleged to be finished products but representing in reality crude forms or semi‑fabricated forms.
1C001 Materials specially designed for absorbing electromagnetic radiation, or intrinsically conductive polymers, as follows:
N.B.: SEE ALSO 1C101.
a. Materials for absorbing frequencies exceeding 2 x 108 Hz but less than 3 x 1012 Hz;
Note 1: 1C001.a. does not apply to:
a. Hair type absorbers, constructed of natural or synthetic fibres, with non‑magnetic loading to provide absorption;
b. Absorbers having no magnetic loss and whose incident surface is non‑planar in shape, including pyramids, cones, wedges and convoluted surfaces;
c. Planar absorbers, having all of the following:
1. Made from any of the following:
a. Plastic foam materials (flexible or non‑flexible) with carbon‑loading, or organic materials, including binders, providing more than 5% echo compared with metal over a bandwidth exceeding ±15% of the centre frequency of the incident energy, and not capable of withstanding temperatures exceeding 450 K (177°C); or
b. Ceramic materials providing more than 20% echo compared with metal over a bandwidth exceeding ±15% of the centre frequency of the incident energy, and not capable of withstanding temperatures exceeding 800 K (527°C);
Absorption test samples for 1C001.a. Note: 1.c.1. should be a square at least 5 wavelengths of the centre frequency on a side and positioned in the far field of the radiating element.
2. Tensile strength less than 7 x 106 N/m2; and
3. Compressive strength less than 14 x 106 N/m2;
d. Planar absorbers made of sintered ferrite, having all of the following:
1. A specific gravity exceeding 4.4; and
2. A maximum operating temperature of 548 K (275°C);
e. Planar absorbers having no magnetic loss and fabricated from ‘open‑cell foam’ plastic material with a density of 0.15 grams/cm3 or less.
‘Open‑cell foams’ are flexible and porous materials, having an inner structure open to the atmosphere. ‘Open‑cell foams’ are also known as reticulated foams.
Note 2: Nothing in Note 1 to 1C001.a. releases magnetic materials to provide absorption when contained in paint.
b. Materials not transparent to visible light and specially designed for absorbing near‑infrared radiation having a wavelength exceeding 810 nm but less than 2000 nm (frequencies exceeding 150 THz but less than 370 THz);
Note: 1C001.b. does not apply to materials, specially designed or formulated for any of the following applications:
a. “Laser” marking of polymers; or
b. “Laser” welding of polymers.
c. Intrinsically conductive polymeric materials with a ‘bulk electrical conductivity’ exceeding 10,000 S/m (Siemens per metre) or a ‘sheet (surface) resistivity’ of less than 100 ohms/square, based on any of the following polymers:
1. Polyaniline;
2. Polypyrrole;
3. Polythiophene;
4. Poly phenylene‑vinylene; or
5. Poly thienylene‑vinylene.
‘Bulk electrical conductivity’ and ‘sheet (surface) resistivity’ should be determined using ASTM D‑257 or national equivalents.
Note: 1C001.c. does not apply to materials in a liquid form.
1C002 Metal alloys, metal alloy powder and alloyed materials, as follows:
N.B.: SEE ALSO 1C202.
Note: 1C002 does not apply to metal alloys, metal alloy powder and alloyed materials, specially formulated for coating purposes.
1. The metal alloys in 1C002 are those containing a higher percentage by weight of the stated metal than of any other element.
2. ‘Stress‑rupture life’ should be measured in accordance with ASTM standard E‑139 or national equivalents.
3. ‘Low cycle fatigue life’ should be measured in accordance with ASTM Standard E‑606 ‘Recommended Practice for Constant‑Amplitude Low‑Cycle Fatigue Testing’ or national equivalents. Testing should be axial with an average stress ratio equal to 1 and a stress‑concentration factor (Kt) equal to 1. The average stress ratio is defined as maximum stress minus minimum stress divided by maximum stress.
a. Aluminides, as follows:
1. Nickel aluminides containing a minimum of 15% by weight aluminium, a maximum of 38% by weight aluminium and at least one additional alloying element;
2. Titanium aluminides containing 10% by weight or more aluminium and at least one additional alloying element;
b. Metal alloys, as follows, made from the powder or particulate material specified by 1C002.c.:
1. Nickel alloys having any of the following:
a. A ‘stress‑rupture life’ of 10,000 hours or longer at 923 K (650°C) at a stress of 676 MPa; or
b. A ‘low cycle fatigue life’ of 10,000 cycles or more at 823 K (550° C) at a maximum stress of 1,095 MPa;
2. Niobium alloys having any of the following:
a. A ‘stress‑rupture life’ of 10,000 hours or longer at 1,073 K (800°C) at a stress of 400 MPa; or
b. A ‘low cycle fatigue life’ of 10,000 cycles or more at 973 K (700°C) at a maximum stress of 700 MPa;
3. Titanium alloys having any of the following:
a. A ‘stress‑rupture life’ of 10,000 hours or longer at 723 K (450°C) at a stress of 200 MPa; or
b. A ‘low cycle fatigue life’ of 10,000 cycles or more at 723 K (450°C) at a maximum stress of 400 MPa;
4. Aluminium alloys having any of the following:
a. A tensile strength of 240 MPa or more at 473 K (200°C); or
b. A tensile strength of 415 MPa or more at 298 K (25°C);
5. Magnesium alloys having all of the following:
a. A tensile strength of 345 MPa or more; and
b. A corrosion rate of less than 1 mm/year in 3% sodium chloride aqueous solution measured in accordance with ASTM standard G‑31 or national equivalents;
c. Metal alloy powder or particulate material, having all of the following:
1. Made from any of the following composition systems:
X in the following equals one or more alloying elements.
a. Nickel alloys (Ni‑Al‑X, Ni‑X‑Al) qualified for turbine engine parts or components, i.e. with less than 3 non‑metallic particles (introduced during the manufacturing process) larger than 100 µm in 109 alloy particles;
b. Niobium alloys (Nb‑Al‑X or Nb‑X‑Al, Nb‑Si‑X or Nb‑X‑Si, Nb‑Ti‑X or Nb‑X‑Ti);
c. Titanium alloys (Ti‑Al‑X or Ti‑X‑Al);
d. Aluminium alloys (Al‑Mg‑X or Al‑X‑Mg, Al‑Zn‑X or Al‑X‑Zn, Al‑Fe‑X or Al‑X‑Fe); or
e. Magnesium alloys (Mg‑Al‑X or Mg‑X‑Al);
2. Made in a controlled environment by any of the following processes:
a. ‘Vacuum atomisation’;
b. ‘Gas atomisation’;
c. ‘Rotary atomisation’;
d. ‘Splat quenching’;
e. ‘Melt spinning’ and ‘comminution’;
f. ‘Melt extraction’ and ‘comminution’;
g. ‘Mechanical alloying’; or
h. ‘Plasma atomisation’; and
3. Capable of forming materials specified by 1C002.a. or 1C002.b.;
d. Alloyed materials having all of the following:
1. Made from any of the composition systems specified by 1C002.c.1.;
2. In the form of uncomminuted flakes, ribbons or thin rods; and
3. Produced in a controlled environment by any of the following:
a. ‘Splat quenching’;
b. ‘Melt spinning’; or
c. ‘Melt extraction’.
1. ‘Vacuum atomisation’ is a process to reduce a molten stream of metal to droplets of a diameter of 500 μm or less by the rapid evolution of a dissolved gas upon exposure to a vacuum.
2. ‘Gas atomisation’ is a process to reduce a molten stream of metal alloy to droplets of 500 μm diameter or less by a high pressure gas stream.
3. ‘Rotary atomisation’ is a process to reduce a stream or pool of molten metal to droplets to a diameter of 500 μm or less by centrifugal force.
4. ‘Splat quenching’ is a process to ‘solidify rapidly’ a molten metal stream impinging upon a chilled block, forming a flake‑like product.
5. ‘Melt spinning’ is a process to ‘solidify rapidly’ a molten metal stream impinging upon a rotating chilled block, forming a flake, ribbon or rod‑like product.
6. ‘Comminution’ is a process to reduce a material to particles by crushing or grinding.
7. ‘Melt extraction’ is a process to ‘solidify rapidly’ and extract a ribbon‑like alloy product by the insertion of a short segment of a rotating chilled block into a bath of a molten metal alloy.
8. ‘Mechanical alloying’ is an alloying process resulting from the bonding, fracturing and rebonding of elemental and master alloy powders by mechanical impact. Non‑metallic particles may be incorporated in the alloy by addition of the appropriate powders.
9. ‘Plasma atomisation’ is a process to reduce a molten stream or solid metal to droplets of 500 μm diameter or less, using plasma torches in an inert gas environment.
10. ‘Solidify rapidly’ is a process involving the solidification of molten material at cooling rates exceeding 1000 K/sec.
1C003 Magnetic metals, of all types and of whatever form, having any of the following:
a. Initial relative permeability of 120,000 or more and a thickness of 0.05 mm or less;
Measurement of initial permeability must be performed on fully annealed materials.
b. Magnetostrictive alloys having any of the following:
1. A saturation magnetostriction of more than 5 x 10‑4; or
2. A magnetomechanical coupling factor (k) of more than 0.8; or
c. Amorphous or ‘nanocrystalline’ alloy strips, having all of the following:
1. A composition having a minimum of 75% by weight of iron, cobalt or nickel;
2. A saturation magnetic induction (Bs) of 1.6 T or more; and
3. Any of the following:
a. A strip thickness of 0.02 mm or less; or
b. An electrical resistivity of 2 x 10‑4 ohm cm or more.
‘Nanocrystalline’ materials in 1C003.c. are those materials having a crystal grain size of 50 nm or less, as determined by X‑ray diffraction.
1C004 Uranium titanium alloys or tungsten alloys with a “matrix” based on iron, nickel or copper, having all of the following:
a. A density exceeding 17.5 g/cm3;
b. An elastic limit exceeding 880 MPa;
c. An ultimate tensile strength exceeding 1,270 MPa; and
d. An elongation exceeding 8%.
1C005 “Superconductive” “composite” conductors in lengths exceeding 100 m or with a mass exceeding 100 g, as follows:
a. “Superconductive” “composite” conductors containing one or more niobium‑titanium ‘filaments’, having all of the following:
1. Embedded in a “matrix” other than a copper or copper‑based mixed “matrix”; and
2. Having a cross‑section area less than 0.28 x 10‑4 mm2 (6 µm in diameter for circular ‘filaments’);
b. “Superconductive” “composite” conductors consisting of one or more “superconductive” ‘filaments’ other than niobium‑titanium, having all of the following:
1. A “critical temperature” at zero magnetic induction exceeding 9.85 K (‑263.31°C); and
2. Remaining in the “superconductive” state at a temperature of 4.2 K (‑268.96°C) when exposed to a magnetic field oriented in any direction perpendicular to the longitudinal axis of conductor and corresponding to a magnetic induction of 12 T with critical current density exceeding 1,750 A/mm2 on overall cross‑section of the conductor;
c. “Superconductive” “composite” conductors consisting of one or more “superconductive” ‘filaments’ which remain “superconductive” above 115 K (‑158.16°C).
For the purpose of 1C005 ‘filaments’ may be in wire, cylinder, film, tape or ribbon form.
1C006 Fluids and lubricating materials, as follows:
b. Lubricating materials containing, as their principal ingredients, any of the following:
1. Phenylene or alkylphenylene ethers or thio‑ethers, or their mixtures, containing more than two ether or thio‑ether functions or mixtures thereof; or
2. Fluorinated silicone fluids with a kinematic viscosity of less than 5,000 mm2/s (5,000 centistokes) measured at 298 K (25°C);
c. Damping or flotation fluids having all of the following:
1. Purity exceeding 99.8%;
2. Containing less than 25 particles of 200 µm or larger in size per 100 ml; and
3. Made from at least 85% of any of the following:
a. Dibromotetrafluoroethane (CAS 25497–30–7, 124–73–2, 27336–23–8);
b. Polychlorotrifluoroethylene (oily and waxy modifications only); or
c. Polybromotrifluoroethylene;
d. Fluorocarbon fluids designed for electronic cooling and having all of the following:
1. Containing 85% by weight or more of any of the following, or mixtures thereof:
a. Monomeric forms of perfluoropolyalkylether‑triazines or perfluoroaliphatic‑ethers;
b. Perfluoroalkylamines;
c. Perfluorocycloalkanes; or
d. Perfluoroalkanes;
2. Density at 298 K (25°C) of 1.5 g/ml or more;
3. In a liquid state at 273 K (0°C); and
4. Containing 60% or more by weight of fluorine.
For the purpose of 1C006:
1. ‘Flash point’ is determined using the Cleveland Open Cup Method described in ASTM D‑92 or national equivalents;
2. ‘Pour point’ is determined using the method described in ASTM D‑97 or national equivalents;
3. ‘Viscosity index’ is determined using the method described in ASTM D‑2270 or national equivalents;
4. ‘Thermal stability’ is determined by the following test procedure or national equivalents:
Twenty ml of the fluid under test is placed in a 46 ml type 317 stainless steel chamber containing one each of 12.5 mm (nominal) diameter balls of M‑10 tool steel, 52100 steel and naval bronze (60% Cu, 39% Zn, 0.75% Sn);
The chamber is purged with nitrogen, sealed at atmospheric pressure and the temperature raised to and maintained at 644 ± 6 K (371 ± 6°C) for six hours;
The specimen will be considered thermally stable if, on completion of the above procedure, all of the following conditions are met:
a. The loss in weight of each ball is less than 10 mg/mm2 of ball surface;
b. The change in original viscosity as determined at 311 K (38°C) is less than 25%; and
c. The total acid or base number is less than 0.40;
5. ‘Autogenous ignition temperature’ is determined using the method described in ASTM E‑659 or national equivalents.
1C007 Ceramic powders, ceramic‑“matrix” “composite” materials and ‘precursor materials’, as follows:
N.B.: SEE ALSO 1C107.
a. Ceramic powders of titanium diboride (TiB2) (CAS 12045‑63‑5) having total metallic impurities, excluding intentional additions, of less than 5,000 ppm, an average particle size equal to or less than 5 µm and no more than 10% of the particles larger than 10 µm;
c. Ceramic‑“matrix” “composite” materials as follows:
1. Ceramic‑ceramic “composite” materials with a glass or oxide‑“matrix” and reinforced with any of the following:
a. Continuous fibres made from any of the following materials:
1. Al2O3 (CAS 1344‑28‑1); or
2. Si‑C‑N; or
Note: 1C007.c.1.a. does not apply to “composites” containing fibres with a tensile strength of less than 700 MPa at 1,273 K (1,000°C) or tensile creep resistance of more than 1% creep strain at 100 MPa load and 1,273 K (1,000°C) for 100 hours.
b. Fibres being all of the following:
1. Made from any of the following materials:
a. Si‑N;
b. Si‑C;
c. Si‑Al‑O‑N; or
d. Si‑O‑N; and
2. Having a “specific tensile strength” exceeding 12.7 x 103m;
2. Ceramic‑“matrix” “composite” materials with a “matrix” formed of carbides or nitrides of silicon, zirconium or boron;
N.B.: For items previously specified by 1C007.c. see 1C007.c.1.b.
N.B.: For items previously specified by 1C007.d. see 1C007.c.2.
e. ‘Precursor materials’ specially designed for the “production” of materials specified by 1C007.c., as follows:
1. Polydiorganosilanes;
2. Polysilazanes;
3. Polycarbosilazanes;
For the purposes of 1C007., ‘precursor materials’ are special purpose polymeric or metallo‑organic materials used for the “production” of silicon carbide, silicon nitride, or ceramics with silicon, carbon and nitrogen.
N.B.: For items previously specified by 1C007.f. see 1C007.c.1.a.
1C008 Non‑fluorinated polymeric substances as follows:
a. Imides as follows:
1. Bismaleimides;
2. Aromatic polyamide‑imides (PAI) having a ‘glass transition temperature (Tg)’ exceeding 563 K (290°C);
3. Aromatic polyimides having a ‘glass transition temperature (Tg)’ exceeding 505 K (232°C);
4. Aromatic polyetherimides having a ‘glass transition temperature (Tg)’ exceeding 513 K (240°C);
Note: 1C008.a. applies to the substances in liquid or solid “fusible” form, including resin, powder, pellet, film, sheet, tape or ribbon.
N.B.: For non‑“fusible” aromatic polyimides in film, sheet, tape or ribbon form, see 1A003.
d. Polyarylene ketones;
e. Polyarylene sulphides, where the arylene group is biphenylene, triphenylene or combinations thereof;
f. Polybiphenylenethersulphone having a ‘glass transition temperature (Tg)’ exceeding 563 K (290°C).
1. The ‘glass transition temperature (Tg)’ for 1C008.a.2. thermoplastic materials, 1C008.a.4. materials and 1C008.f. materials is determined using the method described in ISO 11357‑2 (1999) or national equivalents.
2. The ‘glass transition temperature (Tg)’ for 1C008.a.2. thermosetting materials and 1C008.a.3. materials 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.
1C009 Unprocessed fluorinated compounds as follows:
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 purpose 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 equivalent.
2. 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. 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:
1. A “specific modulus” exceeding 12.7 x 106 m; and
2. A “specific tensile strength” exceeding 23.5 x 104 m;
Note: 1C010.a. does not apply to polyethylene.
b. Carbon “fibrous or filamentary materials”, having all of the following:
1. “Specific modulus” exceeding 14.65 x 106 m; and
2. “Specific tensile strength” exceeding 26.82 x 104 m;
Note: 1C010.b. does not apply to:
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 x 106 m; or
b. Not specified in 1C010.c.1.a. and having a “specific modulus” exceeding 5.6 x 106 m; and
2. Melting, softening, decomposition or sublimation point exceeding 1,922 K (1,649°C) in an inert environment;
Note: 1C010.c. does not apply to:
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 x 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 by 1C008.a.; or
b. Materials specified by 1C008.d. to 1C008.f.; or
2. Composed of materials specified by 1C010.d.1.a. or 1C010.d.1.b. and ‘commingled’ with other fibres specified by 1C010.a., 1C010.b. or 1C010.c.;
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 by 1C010.c.; or
b. Organic or carbon “fibrous or filamentary materials”, having all of the following:
1. “Specific modulus” exceeding 10.15 x 106 m; and
2. “Specific tensile strength” exceeding 17.7 x 104 m; and
a. Resin or pitch, specified by 1C008 or 1C009.b.;
b. ‘Dynamic Mechanical Analysis glass transition temperature (DMA Tg)’ equal to or exceeding 453 K (180ºC) and having a phenolic resin; or
c. ‘Dynamic Mechanical Analysis glass transition temperature (DMA Tg)’ equal to or exceeding 505 K (232ºC) and having a resin or pitch, not specified by 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 apply to:
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 by 1C008. or 1C009.b.
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 by 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 MUNITIONS LIST 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;
The natural content of hafnium in the zirconium (typically 2% to 7%) is counted with the zirconium.
Note: The metals or alloys specified by 1C011.a. also refer to 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;
2. Boron alloys with a boron content of 85% by weight or more;
Note: The metals or alloys specified by 1C011.b. also refer to the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium.
c. Guanidine nitrate;
d. Nitroguanidine (NQ) (CAS 556‑88‑7).
N.B.: SEE ALSO MUNITIONS LIST CONTROLS FOR METAL POWDERS MIXED WITH OTHER SUBSTANCES TO FORM A MIXTURE FORMULATED FOR MILITARY PURPOSES.
1C012 Materials as follows:
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 apply to:
a. Shipments with a plutonium content of 1 g or less;
b. Shipments of 3 ‘effective grams’ or less when contained in a sensing component in instruments.
‘Effective grams’ for plutonium isotope is defined as the isotope weight in grams.
b. ‘Previously separated’ neptunium‑237 in any form.
Note: 1C012.b. does not apply to shipments with a neptunium‑237 content of 1 g or less.
‘Previously separated’ is the application of any process intended to increase the concentration of the controlled isotope.
1C101 Materials and devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures, other than those specified by 1C001, usable in ‘missiles’, ‘missile’ subsystems or unmanned aerial vehicles specified by 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.
1C102 Resaturated pyrolised carbon‑carbon materials designed for space launch vehicles specified by 9A004 or sounding rockets specified by 9A104.
1C107 Graphite and ceramic materials, other than those specified by 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;
2. 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
3. Blocks having a size of 120 mm x 120 mm x 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 by 9A004 or sounding rockets specified by 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 by 9A004 or sounding rockets specified by 9A104;
d. Bulk machinable silicon‑carbide reinforced unfired ceramic, usable for nose tips usable in “missiles”, space launch vehicles specified by 9A004 or sounding rockets specified by 9A104;
e. Reinforced silicon‑carbide ceramic composites, usable for nose tips, reentry vehicles and nozzle flaps usable in “missiles”, space launch vehicles specified by 9A004 or sounding rockets specified by 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 3000°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’.
Note: 1C107.f. does not apply to ‘Ultra High Temperature Ceramic (UHTC)’ materials in non‑composite form.
1. In 1C107.f., ‘missiles’ means complete rocket systems and “unmanned aerial vehicles” capable of a range exceeding 300 km.
2. In 1C107.f., ‘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 by 1C011, as follows:
a. Propulsive substances:
1. Spherical or spheroidal aluminium powder, other than that specified in the Munitions List, 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 2591:1988 or national equivalents;
A particle size of 63 µm (ISO R‑565) corresponds to 250 mesh (Tyler) or 230 mesh (ASTM standard E‑11).
2. Metal powders, other than that specified in the Munitions List, with at least 90% of the total particles by particle volume or weight 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 of any of the following:
a. Zirconium (CAS 7440‑67‑7) or zirconium alloys consisting of 97% by weight or more of zirconium;
b. Beryllium (CAS 7440‑41‑7) or beryllium alloys consisting of 97% by weight or more of beryllium;
c. Magnesium (CAS 7439‑95‑4) magnesium alloys consisting of 97% by weight or more of magnesium; or
d. Boron (CAS 7440‑42‑8) or boron alloys consisting of 85% by weight or more of boron;
Note: In a multimodal particle distribution (e.g. mixtures of different grain sizes) in which one or more modes are controlled, the entire powder mixture is controlled.
The natural content of hafnium in the zirconium (typically 2% to 7%) is counted with the zirconium.
3. 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);
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 MUNITIONS LIST FOR Inhibited Red Fuming Nitric Acid (IRFNA);
f. SEE MUNITIONS LIST AND 1C238 FOR Compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen;
4. Hydrazine derivatives as follows:
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;
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;
l. 2‑hydroxyethylhydrazine nitrate (HEHN);
m. See Munitions List 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);
5. High energy density materials, other than that specified in the Munitions List, usable in ‘missiles’ or unmanned aerial vehicles specified by 9A012 or 9A112.a:
a. Mixed fuel that incorporates both solid and liquid fuels, such as boron slurry, having a mass‑based energy density of 40 x 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 x 109 J/m3 or greater, measured at 20oC and one atmosphere (101.325 kPa) pressure;
Note: 1C111.a.5.b. does not apply to 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 by 9A012 or 9A112.a.
In 1C111.a.5., ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
6. Hydrazine replacement fuels as follows:
a. 1.2‑Dimethylaminoethylazide (DMAZ) (CAS 86147‑04‑8);
2. Hydroxy‑terminated polybutadiene (included hydroxyl‑terminated polybutadiene) (HTPB) (CAS 69102‑90‑5), other than that specified in the Munitions List;
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:
1. SEE MUNITIONS LIST FOR Carboranes, decaboranes, pentaboranes and derivatives thereof;
c. n‑Propyl ferrocene (CAS 1273‑92‑3) / iso‑propyl ferrocene (CAS 12126‑81‑7);
d. See Munitions List for n‑butyl ferrocene;
e. Pentyl ferrocene (CAS 1274‑00‑6);
f. Dicyclopentyl ferrocene;
g. Dicyclohexyl ferrocene;
h. Diethyl ferrocene (CAS 1273–97–8);
i. Dipropyl ferrocene;
j. Dibutyl ferrocene (CAS 1274‑08‑4);
k. Dihexyl ferrocene (CAS 93894‑59‑8);
l. Acetyl ferrocene (CAS 1271–55–2) / 1,1’‑diacetyl ferrocene (CAS 1273–94–5);
m. See Munitions List for ferrocene Carboxylic acids;
n. See Munitions List for butacene;
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 apply to ferrocene derivatives that contain a six carbon aromatic functional group attached to the ferrocene molecule.
7. 4,5 diazidomethyl‑2‑methyl‑1,2,3‑triazole (iso‑ DAMTR) , other than that specified in the Munitions List.
Note: For propellants and constituent chemicals for propellants not specified by 1C111, see the Munitions List.
1C116 Maraging steels having an ultimate tensile strength of 1,500 MPa or greater, measured at 293 K (20°C), in the form of sheet, plate or tubing with a wall or plate thickness equal to or less than 5 mm.
N.B.: SEE ALSO 1C216.
Maraging steels are iron alloys generally characterised by high nickel, very low carbon content and the use of substitutional elements or precipitates to produce strengthening and age‑hardening of the alloy.
1C117 Materials for the fabrication of ‘missile’ 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 x 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 x 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
2. 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.
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:
2. Having a titanium content of greater than 0.10 weight percent; and
3. A ferritic‑austenitic microstructure (also referred to as a two‑phase microstructure) of which at least 10 percent is austenite by volume (according to ASTM E‑1181‑87 or national equivalents); and
b. Having any of the following forms:
1. Ingots or bars having a size of 100 mm or more in each dimension;
2. Sheets having a width of 600 mm or more and a thickness of 3 mm or less; or
3. 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 by 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
2. 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
2. In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm.
The phrase alloys ‘capable of’ encompasses alloys before or after heat treatment.
1C210 ‘Fibrous or filamentary materials’ or prepregs, other than those specified by 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 x 106 m or greater; or
2. A “specific tensile strength” of 235 x 103 m or greater;
Note: 1C210.a. does not apply to aramid ‘fibrous or filamentary materials’ having 0.25 percent or more by weight 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 x 106 m or greater; and
2. A “specific tensile strength” of 76.2 x 103 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 by 1C210.a. or b.
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 by 1C116, ‘capable of’ an ultimate tensile strength of 1,950 MPa or more, at 293 K (20oC).
Note: 1C216 does not apply to 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.
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, 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 apply to manufactures specially designed as weights or gamma‑ray collimators.
1C227 Calcium having both of the following characteristics:
a. Containing less than 1,000 parts per million by weight of metallic impurities other than magnesium; and
b. Containing less than 10 parts per million by weight of boron.
1C228 Magnesium having both of the following characteristics:
a. Containing less than 200 parts per million by weight of metallic impurities other than calcium; and
b. Containing less than 10 parts per million 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 (parts per million) 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 Munitions List controls.
N.B.: SEE ALSO MUNITIONS LIST CONTROLS.
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 apply to 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 apply to thermoluminescent dosimeters.
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.
Note: 1C234 does not apply to 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 1000, and products or devices containing any of the foregoing.
Note: 1C235 does not apply to a product or device containing less than 1.48 x 103 GBq (40 Ci) of tritium.
1C236 Radionuclides appropriate for making neutron sources based on alpha‑n reaction (Actinum 225, Actinum 227, Californium 253, Curium 240, Curium 241, Curium 242, Curium 243, Curium 244, Einsteinium 253, Einsteinium 254, Gadolinium 148, Plutonium 236, Plutonium 238, Polonium 208, Polonium 209, Polonium 210, Radium 223, Thorium 227, Thorium 228, Uranium 230 or Uranium 232) 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 apply to a product or device containing less than 3.7 GBq (100 millicuries) of activity.
1C237 Radium‑226 (226Ra), radium‑226 alloys, radium‑226 compounds, mixtures containing radium‑226, manufactures therof, and products or devices containing any of the foregoing.
Note: 1C237 does not apply to 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 Munitions List, 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 by 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
2. A mean particle size of less than 10 micrometres measured by American Society for Testing and Materials (ASTM) B330 standard;
b. Porous nickel metal produced from materials specified by 1C240.a.
Note: 1C240 does not apply to 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.
N.B.: SEE 0C005 FOR NICKEL POWDERS SPECIALLY PREPARED FOR THE MANUFACTURE OF GASEOUS DIFFUSION BARRIERS.
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, 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 20kg.
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 MUNITIONS LIST AND 1C450.
1. Thiodiglycol (CAS 111‑48‑8);
2. Phosphorus oxychloride (CAS 10025‑87‑3);
3. Dimethyl methylphosphonate (CAS 756‑79‑6);
4. SEE MUNITIONS LIST FOR Methyl phosphonyl difluoride (CAS 676‑99‑3);
Note 1: For exports to “States not Party to the Chemical Weapons Convention”, 1C350 does not apply to “chemical mixtures” containing one or more of the chemicals specified by 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 and .63 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 apply to “chemical mixtures” containing one or more of the chemicals specified by 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 and .63 in which no individually specified chemical constitutes more than 30% by the weight of the mixture.
Note 3: 1C350 does not apply to “chemical mixtures” containing one or more of the chemicals specified by 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 and .65 in which no individually specified chemical constitutes more than 30% by the weight of the mixture.
Note 4: 1C350 does not apply to products identified as consumer goods packaged for retail sale for personal use or packaged for individual use.
1C351 Human pathogens, zoonoses 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. Andes virus;
2. Chapare virus;
3. Chikungunya virus;
4. Choclo virus;
5. Crimean‑Congo haemorrhagic fever virus;
7. Dobrava‑Belgrade virus;
8. Eastern equine encephalitis virus;
9. Ebolavirus (all members of the Ebolavirus genus);
10. Guanarito virus;
11. Hantaan virus;
12. Hendra virus (Equine morbillivirus);
13. Japanese encephalitis virus;
14. Junin virus;
15. Kyasanur Forest disease virus;
16. Laguna Negra virus;
17. Lassa fever virus;
18. Louping ill virus;
19. Lujo virus;
20. Lymphocytic choriomeningitis virus;
21. Machupo virus;
22. Marburgvirus (all members of the Marburgvirus genus);
43. Middle East respiratory syndrome‑related coronavirus (MERS‑CoV);
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;
2. Brucella abortus;
3. Brucella melitensis;
4. Brucella suis;
5. Chlamydophila psittaci (formerly known as Chlamydia psittaci);
6. Clostridium botulinum;
7. Clostridium argentinense (formerly known as Clostridium botulinum Type G), botulinum neurotoxin producing strains;
Note: Limiting this control to epsilon toxin‑producing strains of Clostridium perfringens therefore exempts from control the transfer of other Clostridium perfringens strains to be used as positive control cultures for food testing and quality control.
18. 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).
19. Coxiella burnetii;
20. Rickettsia prowazekii;
d. “Toxins”, as follows, and “sub‑unit of toxins” thereof:
6. Shiga toxins (shiga‑like toxins, verotoxins, and verocytotoxins);
7. Staphylococcus aureus enterotoxins, hemolysin alpha toxin, and toxic shock syndrome toxin (formerly known as Staphylococcus enterotoxin F);
8. Tetrodotoxin;
9. Verotoxin and shiga‑like ribosome inactivating proteins;
10. Microcystins (Cyanoginosins);
11. Aflatoxins;
12. Abrin;
13. Cholera toxin;
14. Diacetoxyscirpenol toxin;
15. T‑2 toxin;
16. HT‑2 toxin;
17. Modeccin;
18. Volkensin;
19. Viscum Album Lectin 1 (Viscumin);
Note 1: 1C351.d does not apply to “immunotoxins”.
Note 2: 1C351.d. does not apply to botulinum toxins or conotoxins in product form meeting all of the following criteria:
a. Are pharmaceutical formulations designed for human administration in the treatment of medical conditions;
b. Are pre‑packaged for distribution as medical products;
c. 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;
2. Coccidioides posadasii.
Note: 1C351 does not apply to “vaccines” or “immunotoxins”.
1C352 Animal 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. African swine fever virus;
2. Avian influenza virus, which are:
a. Uncharacterised; or
b. Defined in Annex I(2) EC Directive 2005/94/EC (O.J. 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
2. 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;
3. Bluetongue virus;
4. Foot‑and‑mouth disease virus;
5. Goatpox virus;
6. Herpes virus (Aujeszky’s disease);
7. Swine fever virus (Hog cholera virus);
8. Rabies virus and all other members of the Lyssavirus genus;
9. Newcastle disease virus;
10. Peste‑des‑petits ruminants virus;
11. Porcine Teschovirus;
12. Rinderpest virus;
13. Sheeppox virus;
14. Teschen disease virus;
15. Vesicular stomatitis virus;
16. Lumpy skin disease virus;
17. African horse sickness virus;
18. Swine vesicular disease virus.
b. Mycoplasmas, 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:
1C353 Any ‘genetically‑modified organism’ which contains, or ‘genetic element’ that codes for any of the following:
a. Any gene or genes specific to any listed virus;
b. Any gene or genes specific to any listed bacterium or fungus, and which:
1. In itself or through its transcribed or translated products represents a significant hazard to human, animal or plant health; or
2. Could ‘endow or enhance pathogenicity’; or
c. Any listed toxins or their sub‑units.
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 synthesized 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. 1C353 does not apply to 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.
4. ‘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: 1C353 applies to the viruses, bacteria, fungi and toxins listed in 1C351, 1C352 and 1C354.
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 tymovirus;
2. 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:
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);
Note 1: 1C450 does not apply to “chemical mixtures” containing one or more of the chemicals specified by entries 1C450.a.1., a.2. and a.3. in which no individually specified chemical constitutes more than 1% by the weight of the mixture.
Note 2: Not used since 2019.
Note 3: 1C450 does not apply to “chemical mixtures” containing one or more of the chemicals specified by 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 apply to 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 Munitions List 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 apply to Fonofos: O‑Ethyl S‑phenyl ethylphosphonothiolothionate (CAS 944‑22‑9).
2. 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.
3. 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 by 1C350;
4. 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 by 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 by 1C350;
Note: 1C450.b.5. does not apply to 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).
6. 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 which is specified by 1C350;
7. See 1C350 for ethyldiethanolamine (CAS 139‑87‑7);
8. Methyldiethanolamine (CAS 105‑59‑9).
Note 1: For exports to “States not Party to the Chemical Weapons Convention”, 1C450 does not apply to “chemical mixtures” containing one or more of the chemicals specified by 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 apply to “chemical mixtures” containing one or more of the chemicals specified by 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 apply to “chemical mixtures” containing one or more of the chemicals specified by 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 apply to products identified as consumer goods packaged for retail sale for personal use or packaged for individual use.