OpenLegislation

Paragraph 1C Equipment, Assemblies and Components

Changes not yet applied. Later legislation changes this provision in ways not yet written into the text below:

Materials

1C001

Materials specially designed for use as absorbers of electromagnetic waves, or intrinsically conductive polymers, as followsf1:

a.

Materials for absorbing frequencies exceeding 2 × 108 Hz but less than 3 × 1012 Hz; except:

  • Materials as follows:

    • Note: Nothing in head a. of this entry releases magnetic materials to provide absorption when contained in paint.

    1. 1.

      Hair type absorbers, constructed of natural or synthetic fibres, with non-magnetic loading to provide absorption;

    2. 2.

      Absorbers having no magnetic loss and whose incident surface is non-planar in shape, including pyramids, cones, wedges and convoluted surfaces;

    3. 3.

      Planar absorbers:

      1. a.

        Made from:

      2. 1.

        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

      3. 2.

        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);

      • Note: Absorption test samples for sub-head a.3.a. of this entry should be a square of side of length at least 5 wavelengths of the centre frequency, and should be positioned in the far field of the radiating element.

      1. b.

        Tensile strength less than 7 × 106 N/m2; and

      2. c.

        Compressive strength less than 14 × 106 N/m2;

    4. 4.

      Planar absorbers made of sintered ferrite, with:

      1. a.

        A specific gravity exceeding 4.4; and

      2. b.

        A maximum operating temperature of 548 K (275°C);

b.

Materials for absorbing frequencies exceeding 1.5 × 1014 Hz but less than 3.7 × 1014 Hz and not transparent to visible light;

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.

  • Note: Bulk electrical conductivity and sheet (surface) resistivity should be determined using ASTM D-257.

1C002

Metal alloys, metal alloy powder or alloyed materials, as followsf2:

  • Note: Entry 1C002 does not specify metal alloys, metal alloy powder or alloyed materials for coating substrates.

a.

Metal alloys, as follows:

1.

Nickel or titanium-based alloys in the form of aluminides, as follows, in crude or semi-fabricated forms:

a.

Nickel aluminides containing 10 weight per cent or more aluminium;

b.

Titanium aluminides containing 12 weight per cent or more aluminium;

2.

Metal alloys, as follows, made from metal alloy powder or particulate material specified in head b. of this entry:

a.

Nickel alloys with:

1.

A stress-rupture life of 10,000 hours or longer at 923 K (650°C) at a stress of 550 MPa; or

2.

A low cycle fatigue life of 10,000 cycles or more at 823 K (550°C) at a maximum stress of 700 MPa;

b.

Niobium alloys with:

1.

A stress-rupture life of 10,000 hours or longer at 1,073 K (800°C) at a stress of 400 MPa; or

2.

A low cycle fatigue life of 10,000 cycles or more at 973 K (700°C) at a maximum stress of 700 MPa;

c.

Titanium alloys with:

1.

A stress-rupture life of 10,000 hours or longer at 723 K (450°C) at a stress of 200 MPa; or

2.

A low cycle fatigue life of 10,000 cycles or more at 723 K (450°C) at a maximum stress of 400 MPa;

d.

Aluminium alloys with a tensile strength of:

1.

240 MPa or more at 473 K (200°C); or

2.

415 MPa or more at 298 K (25°C);

e.

Magnesium alloys with a tensile strength of 345 MPa or more and a corrosion rate of less than 1 mm/year in 3% sodium chloride aqueous solution measured in accordance with ASTM standard G-31;

Notes:

1.

The metal alloys specified in head a. of this entry 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.

3.

Low cycle fatigue life should be measured in accordance with ASTM Standard E-606 ‘Recommended Practice for Constant-Amplitude Low-Cycle Fatigue Testing’. Testing should be axial with an average stress ratio equal to 1 and a stress-concentration factor (Kt) equal to 1. The average stress is defined as maximum stress minus minimum stress divided by maximum stress.

b.

Metal alloy powder or particulate material for materials specified in head a. of this entry, as follows:

1.

Made from any of the following composition systems:

  • Note: 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 micrometre in 109 alloy 15 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); and

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; or

g.

Mechanical alloying;

c.

Alloyed materials, in the form of uncomminuted flakes, ribbons or thin rods produced in a controlled environment by splat quenching, melt spinning or melt extraction, used in the manufacture of metal alloy powder or particulate material specified in head b. of this entry.

1C003

Magnetic metals, of all types and of whatever form, having any of the following characteristics:

a.

Initial relative permeability of 120,000 or more and a thickness of 0.05 mm or less;

  • Note: Measurement of initial permeability must be performed on fully annealed materials.

b.

Magnetostrictive alloys with:

1.

A saturation magnetostriction of more than 5 × 10−4 or

2.

A magnetomechanical coupling factor (k) of more than 0.8; or

c.

Amorphous alloy strips having both of the following characteristics:

1.

A composition having a minimum of 75 weight percent of iron, cobalt or nickel; and

2.

A saturation magnetic induction (Bs) of 1.6 T or more, and:

a.

A strip thickness of 0.02 mm or less; or

b.

An electrical resistivity of 2 × 10−4 ohm cm or more.

1C004

Uranium titanium alloys or tungsten alloys with a matrix based on iron, nickel or copper, with:

a.

A density exceeding 17.5 g/cm3;

b.

An elastic limit exceeding 1,250 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.

Multifilamentary superconductive composite conductors containing one or more niobium-titanium filaments:

1.

Embedded in a matrix other than a copper or copper-based mixed matrix; or

2.

With a cross-section area less than 0.28 × 10−4 mm2 (6 micrometre in diameter for circular filaments);

b.

Superconductive composite conductors consisting of one or more superconductive filaments other than niobium-titanium:

1.

With a critical temperature at zero magnetic induction exceeding 9.85 K (-263.31°C) but less than 24 K (-249.16°C);

2.

With a cross-section area less than 0.28 × 10−4 mm2; and

3.

Which remain in the superconductive state at a temperature of 4.2 K (-268.96°C) when exposed to a magnetic field corresponding to a magnetic induction of 12 T.

1C006

Fluids and lubricating materials, as follows:

a.

Hydraulic fluids containing, as their principal ingredients, any of the following compounds or materials:

1.

Synthetic hydrocarbon oils or silahydrocarbon oils with:

a.

A flash point exceeding 477 K (204°C);

b.

A pour point at 239 K (-34°C) or less;

c.

A viscosity index of 75 or more; and

d.

A thermal stability at 616 K (343°C); or

  • Note: For the purpose of this sub-head, silahydrocarbon oils contain exclusively silicon, hydrogen and carbon.

2.

Chlorofluorocarbons with:

a.

No flash point;

b.

An autogenous ignition temperature exceeding 977 K (704°C);

c.

A pour point at 219 K (-54°C) or less;

d.

A viscosity index of 80 or more; and

e.

A boiling point at 473 K (200°C) or higher;

  • Note: For the purpose of this sub-head, chlorofluorocarbons contain exclusively carbon, fluorine and chlorine.

b.

Lubricating materials containing, as their principal ingredients, any of the following compounds or materials:

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 with a purity exceeding 99.8%, containing less than 25 particles of 200 micrometre or larger in size per 100 ml and made from at least 85% of any of the following compounds or materials:

1.

Dibromotetrafluoroethane;

2.

Polychlorotrifluoroethylene (oily and waxy modifications only); or

3.

Polybromotrifluoroethylene.

Notes:

1.

Flash point is determined using the Cleveland Open Cup Methoddescribed in ASTM D-92.

2.

Pour point is determined using the method described in ASTM D-97.

3.

Viscosity index is determined using the method described in ASTM D-2270.

4.

Thermal stability is determined by the following test procedure: 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 ± 6C) 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 methoddescribed in ASTM E-659.

1C007

Ceramic base materials, non-composite ceramic materials, ceramic-matrix composite materials and precursor materials, as followsf3:

a.

Base materials of single or complex borides of titanium having total metallic impurities, excluding intentional additions, of less than 5,000 ppm, an average particle size equal to or less than 5 micrometre and no more than 10% of the particles larger than 10 micrometre;

b.

Non-composite ceramic materials in crude or semi-fabricated form composed of borides of titanium with a density of 98% or more of the theoretical density; except: Abrasives;

c.

Ceramic-ceramic composite materials with a glass or oxide-matrix and reinforced with fibres from any of the following systems:

1.

Si-N;

2.

Si-C;

3.

Si-Al-O-N; or

4.

Si-O-N;

d.

Ceramic-ceramic composite materials, with or without a continuous metallic phase, containing finely dispersed particles or phases of any fibrous or whisker-like material, where carbides or nitrides of silicon, zirconium or boron form the matrix;

e.

Precursor materials (i.e., special purpose polymeric or metallo-organic materials) for producing any phase or phases of the materials specified in head c. of this entry, as follows:

1.

Polydiorganosilanes (for producing silicon carbide);

2.

Polysilazanes (for producing silicon nitride);

3.

Polycarbosilazanes (for producing ceramics with silicon, carbon and nitrogen components).

1C008

Non-fluorinated polymeric substances, as follows:

a.
1.

Bismaleimides;

2.

Aromatic polyamide-imides;

3.

Aromatic polyimides;

4.

Aromatic polyetherimides having a glass transition temperature (Tg) exceeding 503 K (230°C) as measured by the wet method;

  • Note: This head does not specify non-fusible compression moulding powders or moulded forms.

b.

Thermoplastic liquid crystal copolymers having a heat distortion temperature exceeding 523 K (250°C) measured according to ASTM D-648, method A, with a load of 1.82 N/mm2 and composed of:

1.

Either of the following:

a.

Phenylene, biphenylene or naphthalene; or

b.

Methyl, tertiary-butyl or phenyl substituted phenylene, biphenylene or naphthalene; and

2.

Any of the following acids:

a.

Terephthalic acid;

b.

6-hydroxy-2 naphthoic acid; or

c.

4-hydroxybenzoic acid;

c.

Polyarylene ether ketones, as follows:

1.

Polyether ether ketone (PEEK);

2.

Polyether ketone ketone (PEKK);

3.

Polyether ketone (PEK);

4.

Polyether ketone ether ketone ketone (PEKEKK);

d.

Polyarylene ketones;

e.

Polyarylene sulphides, where the arylene group is biphenylene, triphenylene or combinations thereof;

f.

Polybiphenylenethersulphone.

1C009

Unprocessed fluorinated compounds, as follows:

a.

Copolymers of vinylidene fluoride having 75% or more beta crystalline structure without stretching;

b.

Fluorinated polyimides containing 30% or more of combined fluorine;

c.

Fluorinated phosphazene elastomers containing 30% or more of combined fluorine.

1C010

Fibrous or filamentary materials which may be used in organic matrix, metallic matrix or carbon matrix composite structures or laminates, as followsf4:

a.

Organic fibrous or filamentary materials (except polyethylene) with:

1.

A specific modulus exceeding 12.7 × 106m; and

2.

A specific tensile strength exceeding 23.5 × 104m;

b.

Carbon fibrous or filamentary materials with:

1.

A specific modulus exceeding 12.7 × 106m; and

2.

A specific tensile strength exceeding 23.5 × 104m;

Notes:

1.

Properties for materials described in this head should be determined using Suppliers of Advance Composite Materials Association (SACMA) recommended methods SRM 12 to 17 or Japanese Industrial Standard JIS-R-7601, Paragraph 6.6.2., and based on lot average.

2.

This head does not specify fabric made from fibrous or filamentary materials for the repair of aircraft structures or laminates in which the size of individual sheets does not exceed 50 cm × 90 cm.

c.

Inorganic fibrous or filamentary materials with:

1.

A specific modulus exceeding 2.54 × 106m; and

2.

A melting, decomposition or sublimation point exceeding 1,922 K (1,649°C) in an inert environment;

  • Note: This head does not specify:

a.

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

b.

Molybdenum and molybdenum alloy fibres;

c.

Boron fibres;

d.

Discontinuous ceramic fibres with a melting, decomposition or sublimation point lower than 2,043 K (1,770°C) in an inert environment.

d.

Fibrous or filamentary materials:

1.

Composed of any of the following:

a.

Polyetherimides specified in head a. of entry 1C008; or

b.

Materials specified in heads b., c., d., e. or f. of entry 1C008; or

2.

Composed of materials specified in sub-head d.1. of this entry and commingled with other fibres specified in heads a., b. or c. of this entry;

e.

Resin- or pitch-impregnated fibres (prepregs), metal or carbon-coated fibres (preforms) or carbon fibre preforms, as follows:

1.

Made from fibrous or filamentary materials specified in heads a., b. or c. of this entry;

2.

Made from organic or carbon fibrous or filamentary materials:

a.

With a specific tensile strength exceeding 17.7 × 104 m;

b.

With a specific modulus exceeding 10.15 × 106m;

c.

Not specified in heads a. or b. of this entry; and

d.

When impregnated with materials specified in entry 1C008 or head b. of entry 1C009, or with phenolic or epoxy resins, having a glass transition temperature (Tg) exceeding 383 K (110°C).

  • Note: This head does not specify epoxy resin matrix impregnated carbon fibrous or filamentary materials (prepregs) for the repair of aircraft structures or laminates, in which the size of individual sheets of prepreg does not exceed 50 cm × 90 cm.

1C101

Materials and devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures (i.e. stealth technology), other than those specified in entry 1C001, usable in missiles and their subsystems.

Notes:

1.

This entry 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, infra red or ultra violet regions of the electromagnetic spectrum.

2.

This entry does not include coatings when specially used for the thermal control of satellites.

1C107

Graphite and ceramic materials, as follows:

a.

Fine grain recrystallised bulk graphites, having a bulk density of 1.72 g/cm3 or greater, measured at 288 K (15°C), and having a particle size of 100 micrometres or less, pyrolytic or fibrous reinforced graphites, usable for rocket nozzles and reentry vehicle nose tips;

b.

Ceramic composite materials (dielectric constant less than 6 at frequencies from 100 Hz to 10,000 MHz), usable for radomes, and bulk machinable silicon-carbide reinforced unfired ceramic, usable for nose tips.

1C115

Propellants and constituent chemicals for propellants, as follows:

a.

Propulsive substances:

1.

Spherical aluminium powder, other than that specified in ML8 of Group 1 of Part III of this Schedule, with particles of uniform diameter of less than 500 micrometre and an aluminium content of 97% by weight or greater;

2.

Metal fuels, other than that specified in ML8 of Group 1 of Part III of this Schedule, in particle sizes less than 500 micrometres, whether spherical, atomized, spheroidal, flaked or ground, consisting of 97% by weight or more of any of the following:

a.

Zirconium;

b.

Beryllium;

c.

Boron;

d.

Magnesium;

e.

Zinc;

f.

Alloys of the metals specified by a. to e. above; or

g.

Misch metal;

3.

Liquid oxidisers, the following:

a.

Dinitrogen trioxide;

b.

Nitrogen dioxide/dinitrogen tetroxide;

c.

Dinitrogen pentoxide;

b.

Polymeric substances:

1.

Carboxy-terminated polybutadiene (CTPB);

2.

Hydroxy-terminated polybutadiene (HTPB), other than that specified in ML8 of Group 1 of Part III of this Schedule;

3.

Polybutadiene-acrylic acid (PBAA);

4.

Polybutadiene-acrylic acid-acrylonitrile (PBAN);

c.

Other propellant additives and agents:

1.

Butacene;

2.

Triethylene glycol dinitrate (TEGDN);

3.

2-Nitrodiphenylamine.

  • Note: For propellants and constituent chemicals for propellants not specified here, see ML8 of Group 1 of Part III of this Schedule.

1C116

Maraging steels (steels generally characterised by high nickel, very low carbon content and the use of substitutional elements or precipitates to produce age-hardening) having an ultimate tensile strength of 1500 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 mmf5.

1C117

Tungsten, molybdenum and alloys of these metals in the form of uniform spherical or atomized particles of 500 micrometre diameter or less with a purity of 97% or greater for fabrication of rocket motor components i.e. heat shields, nozzle substrates, nozzle throats and thrust vector control surfaces.

1C202

Alloys, other than those specified in sub-head a.2.c. or head d. of entry 1C002, as follows:

a.

Aluminium alloys capable of an ultimate tensile strength of 460 MPa or more at 293 K (20°C), in the form of tubes or solid forms (including forgings) with an outside diameter of more than 75 mm;

b.

Titanium alloys capable of an ultimate tensile strength of 900 MPa or more at 293 K (20°C) in the form of tubes or solid forms (including forgings) with an outside diameter of more than 75 mm.

  • In this entry, “alloys capable of” means alloys before or after heat treatment.

1C210

Fibrous or filamentary materials, other than those specified in heads a. or b. of entry 1C010, as follows:

a.

Carbon or aramid fibrous or filamentary materials having a specific modulus of 12.7 × 106 m or greater or a specific tensile strength of 23.5 × 104 m or greater; or

b.

Glass fibrous or filamentary materials having a specific modulus of 3.18 × 106 m or greater and a specific tensile strength of 7.62 × 104 m or greater.

1C216

Maraging steel, other than that specified in entry 1C116, capable of an ultimate tensile strength of 2,050 MPa or more, at 293 K (20°C);

  • except:

  • Forms in which no linear dimension exceeds 75 mm.

  • In this entry, “maraging steel capable of” means maraging steel before or after heat treatment.

1C225

Boron and boron compounds, mixtures and loaded materials in which the boron-10 isotope is more than 20% by weight of the total boron content.

1C226

Tungsten, as follows: parts made of tungsten, tungsten carbide, or tungsten alloys (greater than 90% tungsten) having a mass greater than 20 kg and a hollow cylindrical symmetry (including cylinder segments) with an inside diameter greater than 100 mm but less than 300 mm;

  • except:

  • Parts specially designed for use as weights or gamma-ray collimators.

1C227

Calcium (high purity) containing both less than 1,000 parts per million by weight of metallic impurities other than magnesium and less than 10 parts per million of boron.

1C228

Magnesium (high purity) containing both less than 200 parts per million by weight of metallic impurities other than calcium and less than 10 parts per million of boron.

1C229

High purity (99.99% or greater) bismuth with very low silver content (less than 10 parts per million).

1C230

Beryllium metal, alloys containing more than 50% of beryllium by weight, compounds containing beryllium, and manufactures thereof; except:

a.

Metal Windows for X-ray machines;

b.

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

  • Note: This entry includes waste and scrap containing beryllium as defined here.

1C231

Hafnium metal, alloys and compounds of hafnium containing more than 60% hafnium by weight and manufactures thereof.

1C232

Helium in any form isotopically enriched in the helium-3 isotope, whether or not mixed with any other materials or contained in any equipment or device;except:

  • Products or devices containing less than 1 g of helium-3.

1C233

Lithium, as follows:

a.

Metal, hydrides or alloys containing lithium enriched in the 6 isotope (6Li) to a concentration higher than the one existing in nature (7.5 % weight percent);

b.

Any other materials containing lithium enriched in the 6 isotope (including compounds, mixtures and concentrates);

  • except:

  • 6Li incorporated in thermoluminescent dosimeters.

1C234

Zirconium as follows: metal, alloys containing more than 50% zirconium by weight, and compounds in which the ratio of hafnium content to zirconium content is less than 1 part to 500 parts by weight, and manufactures wholly thereof;

  • except:

  • Zirconium in the form of foil having a thickness not exceeding 0.10 mm.

    Notes

    1. 1.

      This entry includes waste and scrap containing zirconium as defined here.

    2. 2.

      For zirconium pressure tubes specially designed or prepared for a nuclear reactor see entry B50 of Group 2 of Part III of this Schedule.

1C235

Tritium, tritium compounds, and mixtures containing tritium in which the ratio of tritium to hydrogen by atoms exceeds 1 part in 1000;

  • except:

  • A product or device containing not more than 40 Ci of tritium in any chemical or physical form.

1C236

Alpha-emitting radionuclides having an alpha half-life of 10 days or greater but less than 200 years, including equipment, compounds and mixtures containing these radionuclides with a total alpha activity of 1 curie per kilogram (37 GBq/kg) or greater;

  • except:

  • Devices containing less than 100 millicuries (3.7 GBq) of alpha activity per device.

1C237

Radium-226;

  • except:

  • Radium contained in medical applicators.

1C238

Chlorine trifluoride (ClF3).

1C239

High explosivesf6, other than those specified in ML8 of Group 1 of Part III of this Schedule, or substances or mixtures containing more than 2% thereof, with a crystal density greater than 1.8 gm/cm3 and having a detonation velocity greater than 8,000 m/s.

1C350

Chemicals, which may be used as precursors for toxic chemical agents, as follows, and preparations thereoff7:

a.
1.

Ammonium hydrogen fluoride;

2.

Arsenic trichloride;

3.

Benzilic acid;

4.

2-Chloroethanol;

5.

Diethylaminoethanol;

6.

Diethyl ethylphosphonate;

7.

Diethyl methylphosphonite;

8.

Diethyl-N,N-dimethylphosphoramidate;

9.

Diethyl phosphite;

10.

Diisopropylamine;

11.

N,N-Diisopropyl-(beta)-aminoethane thiol;

12.

N,N-Diisopropyl-(beta)-amino ethanol;

13.

N,N-Diisopropyl-(beta)-aminoethyl chloride;

14.

N,N-Diisopropyl-(beta)-aminoethyl chloride hydrochloride;

15.

Dimethyl ethylphosphonate;

16.

Dimethyl methylphosphonate;

17.

Dimethyl phosphite;

18.

Dimethylamine;

19.

Dimethylamine hydrochloride;

20.

Ethyl phosphinyl dichloride;

21.

Ethyl phosphinyl difluoride;

22.

Ethyl phosphonyl dichloride;

23.

Ethyl phosphonyl difluoride;

24.

Hydrogen fluoride;

25.

3-Hydroxy-1-methylpiperidine;

26.

Methyl benzilate;

27.

Methyl phosphinyl dichloride;

28.

Methyl phosphinyl difluoride;

29.

Methyl phosphonyl dichloride;

30.

Phosphorus oxychloride;

31.

Phosphorus pentachloride;

32.

Phosphorus pentasulphide;

33.

Phosphorus trichloride;

34.

Pinacolone;

35.

Pinacolyl alcohol;

36.

Potassium fluoride;

37.

Potassium cyanide;

38.

Potassium hydrogen fluoride;

39.

3-Quinuclidinol;

40.

3-Quinuclidone;

41.

Sodium bifluoride;

42.

Sodium cyanide;

43.

Sodium fluoride;

44.

Sodium sulphide;

45.

Sulphur dichloride;

46.

Sulphur monochloride;

47.

Thiodiglycol;

48.

Thionyl chloride;

49.

Triethanolamine;

50.

Triethanolamine hydrochloride;

51.

Triethyl phosphite;

52.

Trimethyl phosphite;

  • except:

  • Preparations which include any of the above chemicals, which;

    1. 1.

      Are put up for retail sale and intended for individual personal use or consumption; or

    2. 2.

      Contain the chemical in such a way that it cannot be easily recovered by standard processes.

1C351

Human pathogens, zoonoses and toxins f8:

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.

Chikungunya virus;

2.

Congo-Crimean haemorrhagic fever virus;

3.

Dengue fever virus;

4.

Eastern equine encephalitis virus;

5.

Ebola virus;

6.

Hantaan virus;

7.

Junin virus;

8.

Lassa fever virus;

9.

Lymphocytic choriomeningitis virus;

10.

Machupo virus;

11.

Marburg virus;

12.

Monkey pox virus;

13.

Rift Valley fever virus;

14.

Russian Spring-Summer encephalitis virus;

15.

Variola virus;

16.

Venezuelan equine encephalitis virus;

17.

Western equine encephalitis virus;

18.

White pox;

19.

Yellow fever virus;

20.

Japanese encephalitis virus;

b.

Rickettsiae, 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.

Coxiella burnetii;

2.

Rickettsia quintana;

3.

Rickettsia prowasecki;

4.

Rickettsia rickettsii;

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.

Chlamydia psittaci;

6.

Clostridium botulinum;

7.

Francisella tularensis;

8.

Pseudomonas mallei (Burkholderia mallei);

9.

Pseudomonas pseudomallei (Burkholderia pseudomallei;

10.

Salmonella typhi;

11.

Shigella dysenteriae;

12.

Vibrio cholerae;

13.

Pasteurella pseudotuberculosis var pestis (Yersinia pestis);

d.

Toxins, as follows;

1.

Botulinum toxins;

2.

Clostridium perfringens toxins;

3.

Conotoxin;

4.

Ricin;

5.

Saxitoxin;

6.

Shiga toxin;

7.

Staphylococcus aureus toxins;

8.

Tetrodotoxin;

9.

Verotoxin;

10.

Microcystins (Cyanginosins);

  • except:

  • Any goods specified in this entry in the form of a vaccinef9.

1C352

Animal Pathogens, as followsf10:

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.

Those defined in Council Directive 92/40/EECf11, 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 H5 or H7 subtype for which nucletide sequencing has demonstrated multiple basic amino acids at the cleavage site of haemagglutinin;

3.

Bluetongue virus;

4.

Foot and mouth disease virus;

5.

Goat pox virus;

6.

Porcine herpes virus (Aujeszky’s disease);

7.

Swine fever virus (Hog cholera virus);

8.

Lyssa virus;

9.

Newcastle disease virus;

10.

Peste des petits ruminants virus;

11.

Swine vesicular disease (porcine enterovirus type 9);

12.

Rinderpest virus;

13.

Sheep pox virus;

14.

Teschen disease virus;

15.

Vesicular stomatitis virus;

b.

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 Mycoplasma mycoides;

  • except:

  • Any goods specified in this entry in the form of a vaccine.

1C353

Genetically-modified microorganisms, as followsf12:

a.

Genetically modified microorganisms or genetic elements that contain nucleic acid sequences associated with pathogenicity and are derived from organisms specified in heads a. to c. of entry 1C351 or entries 1C352 or 1C354;

b.

Genetically modified microorganisms or genetic elements that contain nucleic acid sequences coding for any of the toxins specified in head d. of entry 1C351.

1C354

Plant pathogens, as follows:

a.

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

1.

Xanthomonas albilineans;

2.

Xanthomonas campestris pv. citri including strains referred to as Xanthomonas campestris pv. citri types A,B,C,D,E or otherwise classified as Xanthomonas citri, Xanthomonas campestris pv. aurantifolia or Xanthomonas campestris pv. citrumelo;

b.

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 coffeanum var. virulans;

2.

Cochlibolus miyabeanus (Helminthosporium oryzae);

3.

Microcyclus ulei(syn. Dothidella ulei);

4.

Puccinia graminis (syn. Puccinia graminis f. sp. tritici);

5.

Puccinia striiformis (syn. Puccinia glumarum);

6.

Magnaporthe grisea (Pyricularia grisea/Pyricularia oryzae).

1C991

Other explosives and propellants and related substances as followsf13:

a.

Amatol;

b.

Nitrocellulose (containing more than 12.5% nitrogen);

c.

Nitroglycol;

d.

Pentaerythritol tetranitrate (PETN);

e.

Picryl chloride;

f.

Trinitrophenylmethylnitramine (tetryl);

g.

2,4,6-Trinitrotoluene (TNT).

1C992

Vaccines for protection against either of the following:

a.

Bacillus anthracis; or

b.

Botulinum toxin.

Annotations

Footnotes

f1

See also entry 1C101.

f2

See also entry 1C202.

f3

See also entry 1C107.

f4

See also entry 1C210.

f5

See also entry 1C216.

f6

See also entry 1C991.

f7

See also ML7 of Group 1 of Part III of this Schedule.

f8

See also ML7 of Group 1 of Part III of this Schedule.

f9

See also entry 1C992.

f10

See also ML7 of Group 1 of Part III of this Schedule.

f11

O.J. No. L167, 22.6.92 p.1.

f12

See also ML7 of Group 1 of Part III of this Schedule.

f13

See also entries 1C115, 1C239 and ML8 of Group 1 of Part III of this Schedule.