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The Export of Goods (Control) Order 1987

Type Statutory-Instrument
Publication 1987-11-26
State In force
Department Queen's Printer of Acts of Parliament
Source legislation.gov.uk
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articles Not indexed
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GROUP 3H

Note Goods specified in the heads of this Group may also be specified in Group 2 of this Part of this Schedule.

In this Group, the following definitions apply– Crude forms Anodes, balls, bars (including notched bars and wire bars) billets, blocks, blooms, briquettes, cakes, cathodes, crystals, cubes, dice, grains, granules, ingots, lumps, pellets, pigs, powder, rondelles, shot, slabs, slugs, sponge, sticks;
Semi-fabricated forms (whether or not coated, plated, drilled or punched)– Wrought or worked material fabricated by rolling, drawing, extruding, forging, impact extruding, pressing, graining, atomising and grinding, i.e. angles, channels, circles, discs, dust, flakes, foil and leaf, forgings, plates, powder, pressings and stampings, ribbons, rings, rods (including bare welding rods, wire rods and rolled wire), sections, shapes, sheets, strip, pipe and tube (including tube rounds, squares and hollows), drawn or extruded wire;
2 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.
IL1603 Seamless tubes and pipes having an outside diameter of 60 mm or more, and seamless fittings therefor, made of nickel-base superalloys containing the following major alloying elements, by weight: 19% or more of chronium, 7.4% or more of molybdenum, not more than 6% of iron, and 3% or more of niobium (columbium) or of niobium and tantalum combined A
IL1631 Magnetic materials, the following–
1 Magnetic materials in all forms having any of the following characteristics–
a initial permeability of 0.15 henry/m units (120,000 gauss/oersteds) or more calculated at induction 0 and magentic field strength 0 or the equivalent A
b remanence 98.5% or more of maximum flux for materials having magnetic permeability A
or
c a composition capable of an energy product of 200,000 joules/mu23 (25 x 10u26 gauss-oersteds) or more A
2 Grain oriented iron alloy sheets or strips having a thickness of 0.1 mm or less A
3 Magnetorestrictive alloys having either of the following characteristics–
a saturation magnetorestriction more than 5 × 10u2–u24; or A
b magnetomechanical coupling factor (K) more than 0.8 A
4 Amorphous alloy strips having both of the following characteristics– A
a a composition having 75% or more of iron, cobalt or nickel, and
b a saturation magentic induction of 1.6 tesla or more, with a strip thickness of 0.020 mm or less or electrical resistivity of 2 × 10u2–u24 ohm-cm or more.
IL1635 Steels in crude or semi-fabricated forms containing a higher percentage of iron than of any element and not being products obtained by casting with a carbon content of more than 1.5%, the following–
1 Steels containing 10% or more of molybdenum A
2 Steels containing 5% or more of molybdenum together with 14% or more of chromium A
3 Steel alloys containing a combination of the following major alloy elements in the amounts specified, by weight: 4.5 to 5.95% of nickel, 0.3 to 1.0% of chromium, 0.2 to 0.75% of molybdenum, 0.04 to 0.15% of vanadium and less than 0.19% of carbon A
IL1648 Cobalt-based alloys containing a higher percentage of cobalt than of any other element and one or more of the following constituents in the proportions stated–
1 5% or more of tantalum; or A
2 1% or more of thorium, aluminium, yttrium, zirconium or cerium oxides; or. A
3 0.05% or more of rare earth metals A
in crude or semi-fabricated forms.
IL1649 Niobium (columbium) based alloys containing 60% or more but not more than 99.3% of niobium, or having a combined content of 60% or more but not more than 99.3% of niobium-tantalum, in crude, semi-fabricated or scrap forms A
IL1658 Molybdenum alloys containing not less than 97.5% or more than 99.9% of molybedenum, in crude or semi-fabricated forms, except wire A
IL1661 Nickel alloys containing a higher percentage of nickel than of any other element and containing–
1 11% or more of aluminium and titanium combined; or A
2 1% or more of oxides of thorium, aluminium, yttrium, zirconium, cerium, or lanthanum; or A
3 0.05% or more of scandium, yttrium, didymium, cerium, lanthanum, neodymium or praseodymium A
in crude or semi-fabricated forms.
IL1670 Tantalum, the following–
1 Tantalum powder containing less than 200 parts per million of total metallic impurities A
2 Sintered anodes fabricated from tantalum powder containing less than 200 parts per million of total metallic impurities A
3 Tantalum based alloys containing 60% or more of tantalum (except ferro-tantalum or ferro-tantalum-niobium containing 25% or more of iron or other metalloid elements), in crude or semi-fabricated forms or scrap A
IL1671 Titanium based alloys in crude or semi-fabricated form or scrap, having nominal compositions of 6% aluminium, 2% tin, 4% zirconium, 6% molybdenum and the balance titanium A
In this entry the alloying compositions are nominal and may be subject to slight variations.
IL1672 Aluminides of titanium containing 12% or more of aluminium by weight, and aluminides of nickel, cobalt and iron containing 10% or more of aluminium by weight, in crude or semi-fabricated forms, and scrap thereof A
IL1674 Vanadium, including scrap, of a purity of 99.7% or higher and alloys containing vanadium, including scrap, of such purity as an alloying agent A
IL1675 Superconductive materials of all types and processed conductors containing at least one superconducting constituent, designed for operation at temperatures below 103 K (–170°C) A
except processed conductors possessing all of the following characteristics–
1 The superconducting constituent, when evaluated in sample length of less than 1 metre, does not remain in the superconducting state when exposed to a magnetic induction in excess of 12 tesla at a temperature of 4.2 K (–268°C);
2 The superconducting constituent or filament has a cross-section area greater than 3.14 × 10u2–u24 mmu22 or, in the case of circular filaments, a diameter greater than 20 micrometres;
3 The superconducting filaments are included in a copper or copper-based matrix; and
4 The conductor is either non-coated or insulated with varnish, glass fibre, polyamide or polyimide.
— Aluminium alloys, in which zinc predominates by weight over any other single alloying element in the following forms–
tubes, rods, forgings, bars and billets A
— Maraging steel alloy capable of ultimate tensile strength of 2.050 × 10u29 N/mu22 (300,000 pounds per square inch) or greater, whether or not finally heat-treated, in crude, semi-fabricated or fabricated form A

GROUP 3I — Chemicals, Metalloids and Petroleum Products

IL1702 Hydraulic fluids containing as the principal ingredients petroleum (mineral) oils, synthetic hydrocarbon oils, non-fluorinated silicones or fluorocarbons and having all of the following characteristics– A
1 A flash point of more than 477 K (204°C);
2 A pour point of 239 K (–34°C) or lower;
3 A viscosity index of 75 or greater; and
4 Thermally stable at 616 K (+343°C).
IL1715 Boron, boron compounds, mixtures and alloys, except pharmaceutical preparations packaged for retail sale, the following–
1 Boron element (metal) in all forms A
2 Boron compounds, mixtures and composites containing 5% or more of boron, the following–
a non-ceramic boron-nitrogen compounds A
b boron hydrides, except sodium boron hydride, potassium boron hydride, monoborane, diborane and triborane A
c organoboron compounds including metallo-organoboron compounds A
— Boron compounds and mixtures in which the boron –10 isotope comprises more than 20% of the total boron content A
IL1733 Base materials, non-composite ceramic materials, ceramic-ceramic composite materials and precursor materials for the manufacture of high temperature fine technical ceramic products, the following–
1 Base materials, namely high purity fine powders with uniform particle-size distribution, the following–
single or complex non-composite oxides, borides, carbides or nitrides of silicon, aluminium, boron, zirconium or tantalum A
except
a single oxides of silicon, boron, aluminium or tantalum;
b single or complex borides of silicon; and
c single or complex borides or carbides of aluminium.
2 Non-composite ceramic materials, in crude or semi-fabricated form, having compositions of the base materials specified, other than as exceptions, in head (1) above A
3 Granular or fibrous ceramic-ceramic composite materials containing finely dispersed particles or phases of any non-metallic fibrous or whisker-like materials, whether externally introduced or grown in situ during processing, in which the following materials form the host matrix–
a all oxides, includes glasses A
b carbides or nitrides of silicon or boron A
c borides, carbides or nitrides of zirconium, hafnium or tantalum A
d carbon A
e any combination of these materials A
4 Precursor materials, namely special purpose polymeric or metallo-organic materials for producing any phase or phases of the materials specified in heads (2) or (3) above, the following–
a polycarbosilanes and polydiorganosilanes, for producing silicon carbide A
b polysilazanes, for producing silicon nitride A
c polycarbosilazanes, for producing ceramics with silicon, carbon and nitrogen components A
In this entry, “high purity” means that a powder has a total metallic impurity, excluding intentional or desired additions, of less than 1000 ppm for single oxides or single carbides or less than 5000 ppm for complex compounds, single borides or single nitrides; and “fine powders with uniform particle-size distribution” means powders with at least 90% of the particles being not more than 10 micrometres and the average particle size not more than 5 micrometres. (For zircons, these limits are 5 micrometres and 1 micrometre respectively).
IL1734 Low density, rigid, carbon-bonded fibrous or non-fibrous carbon thermal insulating materials having all of the following characteristics– A
1 a capability of operating at temperatures greater than 2273 K (2000°C);
2 a density greater than 100kg/mu23 and less than 300kg/mu23;
3 a compressive strength of greater than 0.1 MPa and less than 1.0 MPa;
4 a flexural strength of greater than 1.0 MPa; and
5 a carbon content of greater than 99.9% of total solids.
IL1746 Polymeric materials and manufactures thereof, the following–
1 Polyimides (including maleimides) A
except the following forms: fully cured polyimide or polyimide-based film, sheet, tape or ribbon having a maximum thickness of 0.25 mm, whether or not coated or laminated with heat-sensitive or pressure-sensitive resinous substance of an adhesive nature, which contain no fibrous reinforcing materials and which have not been coated or laminated with carbon, graphite, metals or magnetic substances.
2 Polybenzimidazoles A
3 Aromatic polyamides, except staple fibres, filament yarns, chopped fibres, spun yarns or threads, having a fibre modulus of 0.022 Newtons per tex or less and a tenacity of 0.970 Newtons per tex or less, and pulp made from those materials A
4 Polybenzothiazoles A
5 Polyoxadiazoles A
6 Polyphosphonitriles A
7 Polystyrylpyridine A
8 Thermoplastic liquid crystal copolyesters, the following–
a ethylene copolyesters of terephthalic acid and parahydroxybenzoic acid A
except manufactures thereof having both of the following characteristics–
i a tensile modulus of less than 15 GPa; and
ii specially designed for non-aerospace, non-electronic civil applications
b phenylene or biphenylene copolyesters of terephthalic acid and parahydroxybenzoic acid A
9 Polybenzoxazoles A
10 Aromatic polyether ether ketones A
In this entry–
“tenacity” is the tensile stress expressed as force per unit linear density of the unstrained specimen, expressed in Newtons per tex;
“fibre modulus” is the ratio of change in stress to change in strain between two points on a stress-strain curve, viz the point of zero stress and the point of breaking stress expressed in Newtons per tex; and
“tex” is the number of grammes in 1,000 metres of material.
IL1749 Polycarbonate sheet of a thickness between 1.5 mm and 25.4 mm (inclusive) having no major defects and having all of the following optical characteristics– A
1 Less than 2% haze as determined by method ASTM D1003–
2 An angular deviation, as determined by method ASTM D637–
a of not more than 12 minutes at any location more than 25.4 mm from the edge of the sheet for sheet thickness of between 1.5 mm and 9.5 mm (inclusive); or
b of not more than 20 minutes at any location more than 25.4 mm from the edge of the sheet for sheet thickness of more than 9.5 mm and not more than 25.4 mm;
3 A total number of minor optical defects (excluding those within 25.4 mm of the sheet edge)–
a not exceeding 1 per 0.368 mu22 for sheet of a thickness of 12.7 mm or less;
b not exceeding 2 per 0.092 mu22 for sheet of a thickness of more than 12.7 mm.
In this entry “major defects” means variations in the material which cause angular deviations either side of the undeviated position exceeding those specified in head (2) and “minor defects” include any embedded particles, bubbles, scratches or internal inhomogeneity which reduce visibility through the plastic and those localised imperfections which cause a variation in angular deviation of more than 5 minutes within a distance of not more than 508 mm on the screen when tested by method ASTM D637.
IL1754 Fluorinated compounds, materials and manufactures, the following–
1
a Dibromotetrafluorethane, except dibromotetrafluoroethane having a purity of 99.8% or less and containing at least 25 particles each 200 micrometres or larger per 100 ml A
b Perfluoroalkylamines A
2 Polymeric materials and intermediates, unprocessed, the following–
a Polychlorotrifluoroethylene, oily and waxy modifications only A
b Fluoroelastomers composed of at least 95% of a combination of two or more of the monomers tetrafluoroethylene, chlorotrifluoroethylene, vinylidenefluoride, hexafluoropropylene and bromotrifluoroethylene, iodotrifluoroethylene, perfluoromethyl-vinylether and perfluoropropoxy-propylvinylether A
c Polybromotrifluoroethylene A
d Copolymers of vinylidene fluoride having 75% or more beta crystalline structure without stretching A
e Fluorinated silicone rubber and intermediates for their production containing 10% or more of combined fluorine A
3 Greases, lubricants and dielectric, damping and flotation fluids made of at least 85% of any of the materials listed in heads (1) and (2) above; A
4 Electric wire and cable coated with or insulated with any of the materials in (2)(b), except oil well logging cable; A
5 Seals, gaskets, rods, sheets, sealants or fuel bladders made of more than 50% of any of the materials in (2)(b) specially designed for aerospace and aircraft use; A
6 Piezoelectric polymers and copolymers made from vinylidene fluoride having both of the following characteristics– A
a In sheet or film form; and
b With a thickness of more than 200 micrometres.
IL1755 Silicone fluids and greases, the following–
1 Fluorinated silicone fluids, except those with a kinematic viscosity of 5000 centistokes or more measured at 25°C A
2 Silicone and fluorinated silicone lubricating greases capable of operating at temperatures of 180°C or higher and having a drop point of 220°C or higher A
IL1757 Compounds and Materials, the following–
1 Monocrystalline silicon, except metallurgical grade monocrystalline silicon having a purity not better than 99.97% A
2 Gallium of a purity of 99.9999% or greater and gallium III/V compounds of any purity level, A
except
a gallium phosphide; or
b other gallium III/V compounds having a dislocation density (etch pit density – EPD) greater than 500,000 per cmu22;
3 Indium of a purity greater than 99.9995% and III-V indium compounds containing more than 1% indium A
4 Hetero-epitaxial materials consisting of a monocrystalline insulating sub-strate epitaxially layered with silicon, compounds of gallium or compounds of indium A
5 Elemental Cd and Te of purity levels of 99.9995% or greater, and CdTe compounds of a purity level of 99.99% or greater or single crystals of CdTe of any purity level A
6 Polycrystalline silicon, except polycrystalline silicon having a purity of 99.99% or less and containing at least 0.5 part in 10u26 each of iron, carbon, boron and phosphorus, plus other impurities A
(See also the entry in Group 3D relating to equipment for the manufacture of electronic materials.)
7 Compounds used in the synthesis of the materials specified in head (6) above, having a purity level based upon the amount the primary constituent of 99.5% or better, or used as the silicon source in the deposition of epitaxial layers of silicon, silicon oxide or silicon nitride A
This item includes SiCld22Hd22 having a purity level of 97% or more.
8 Single crystal sapphire substrates A
9 Bd22Od23 with a purity of 99.9% or greater, containing 1,000 parts per million of Hd22O or less, in powder or cast form A
10 Monocrystalline germanium with a resistivity greater than 100 ohm. cm. A
11 Resist materials having any of the following characteristics:
a negative resists with a spectral response adjusted for use below 350 nanometres A
b for use with electron or ion beams with a sensitivity of 100 microcoulombs/cmu22 or better A
c positive resists A
d for use with X rays with a sensitivity of 500 millijoules/cmu22 or better; or A
e specified or optimised for dry development A
12 Single-crystal forms of bismuth germanium oxide having piezo-electric properties and single-crystal forms of lithium niobate, of lithium tantalate and of aluminium phosphate A
13 Metal-organic or hydride compounds of beryllium and magnesium, zinc, cadmium and mercury, aluminium, gallium and indium, phosphorus, arsenic and antimony and selenium and tellurium, having a purity (metal basis) of 99,999% or greater A
IL1759 Syntactic foam for underwater use, the following–
1 Syntactic foam formulated for applications at depths greater than 1,000 metres A
2 Syntactic foam having a density of 0.561 g/cmu23 (35 lb/cu.ft.) or less A
In this entry– “syntactic foam” consists of hollow plastic or glass spheres less than 100 micrometres in diameter uniformly embedded in a resin matrix.
IL1760 Compounds of tantalum and niobium (columbium), the following–
1 Tantalates and niobates having a purity of 99% or more, except fluorotantalates A
2 Other compounds containing 20% or more of tantalum in which the niobium content with respect of tantalum is less than 1 part per thousand A
This entry does not cover single-crystal lithium tantalate for which see the entry in this Group relating to compounds and materials.
IL1763 Fibrous and filamentary materials suitable for use in composite structures or laminates, the following–
1 having both of the following characteristics– A
a specific modulus greater than 3.18 × 10u26m (1.25 × 10u28 in);
b specific tensile strength greater than 7.62 × 10u24m (3 × 10u26 in); or
2 having both of the following characteristics– A
a specific modulus greater than 2.54 × 10u26m (1 × 10u28 in);
b melting or sublimation point higher than 1,922 K (1,649°C) in an inert environment;
except
i carbon fibres having a specific modulus less than 5.08 × 10u26m (2 × 10u28 in) and a specific tensile strength less than 2.54 × 10u24m (1 × 10u28 in);
ii discontinuous, multiphase, polycrystalline alumina fibres in chopped fibre or random mat form, containing 3% or more silica, having a specific modulus less than 10 × 10u26m (3.92 × 10u28 inches).
3 Resin-impregnated fibres (prepregs) and metal-coated fibres (preforms) made with materials specified in heads (1) or (2) above A
4 Composite structures, laminates and manufactures thereof made either with an organic matrix or a metal matrix utilising materials specified in heads (1) and (2) above A
In this entry–
“specific modulus” means Young’s modulus in N/mu22 (lb force/sq.in) divided by specific weight in N/mu23 (lb force/cu.in), measured at a temperature of (296 .266 2) K ((23 .266 2)°C) ((73.4 .266 3.6)°F) and a relative humidity of (50 .266 5)%; and
“specific tensile strength” means ultimate tensile strength in N/mu22 (lb force/sq. in) divided by specific weight in N/mu23 (lb force/cu. in) measured at a temperature of (296 .266 2) K ((23 .266 2)°C) ((73.4 .266 3.6)°F) and a relative humidity of (50 .266 5)%.
IL1767 Preforms of glass, or of any other material, specially designed for the fabrication of optical fibres specified in head (2) of the entry in Group 3F relating to cable and wire A
In this entry “preforms” are defined as bars, ingots or rods, of glass, plastic or other materials, which have been specially processed for use in the fabrication of optical fibres.
IL1781 Lubricating oils and greases, synthetic, which are or contain as their principal ingredient, the following–
1 monomeric and polymeric forms of perfluorotriazines, perfluoroaromatic ethers and esters, and perfluoroaliphatic ethers and esters A
2 polyphenyl ethers and thio ethers containing more than three groups of any of the following: A
a phenyl;
b alkyl phenyl;
c phenyl and alkyl phenyl;
— Chemicals, the following–
1 Chloreothanol I
2 Dimethylamine I
3 Dimethyl methylphosphonate A
4 Dimethylphosphite A
5 Hydrogen fluoride A
6 Methyl phosphonyl dichloride A
7 Methyl phosphonyl difluoride A
8 Phosphorus oxychloride A
9 Phosphorus trichloride A
10 Potassium fluoride I
11 Thiodiglycol A
12 Trimethylphosphite A
— Synthetic rubbers, the following–
1 Polymeric products of butadiene, the following:
a carboxyl terminated polybutadiene, hydroxyl terminated polybutadiene, thiol terminated polybutadiene and cyclised 1, 2-polybutadiene A
b mouldable copolymers of butadiene and acrylic acid A
c mouldable terpolymers of butadiene, acrylonitrile and acrylic acid or any of the homologues of acrylic acid A
2 Carboxyl terminated polyisoprene A

GROUP 4 — GOODS, TECHNOLOGIES AND PROCESSES IN RESPECT OF WHICH THE EXPORT OF TECHNOLOGICAL DOCUMENTS, OTHER THAN DOCUMENTS GENERALLY AVAILABLE TO THE PUBLIC, IS PROHIBITED TO ANY DESTINATION IN ANY COUNTRY SPECIFIED IN ARTICLE 2(iv)

IL1001 Technology for metal-working manufacturing processes and specially designed software, the following–
1 Technology for the design of tools, dies and fixtures specially designed for the following processes–
a hot die forging;
b superplastic forming;
c diffusion bonding;
d metal powder compaction using–
i vacuum hot pressing;
ii high pressure extrusion;
iii isostatic pressing;
e direct-acting hydraulic pressing.
2 Technical data consisting of the following process parameters–
a for controlling hot die forging–
i temperature;
ii strain rate;
b for controlling superplastic forming of aluminium alloys, titanium alloys and superalloys–
i surface preparation;
ii strain rate;
iii temperature;
iv pressure;
c for controlling diffusion bonding of superalloys and titanium alloys–
i surface preparation;
ii temperature;
iii pressure;
d for controlling metal powder compaction using vacuum hot pressing, high pressure extrusion or isostatic pressing–
i temperature;
ii pressure;
iii cycle time;
e for controlling direct-acting hydraulic pressing of aluminium alloys for titanium alloys–
i pressure;
ii cycle time;
f for controlling hot isostatic densification of titanium alloys, aluminium alloys and superalloys–
i temperature;
ii pressure;
iii cycle time.
IL1080 Technology, other than installation, operation and maintenance technology, for the use of the following equipment used in the manufacture of gas turbine blades or vanes–
1 Blade or vane belt grinding machines;
2 Blade or vane edge radiusing machines;
3 Blade or vane aerofoil milling or grinding machines;
4 Blade or vane blank preforming machines;
5 Blade or vane rolling machines;
6 Blade or vane aerofoil shaping machines, except metal removing types;
7 Blade or vane root grinding machines; and
8 Blade or vane aerofoil scribing equipment.
IL1372 Technology common to industrial gas turbine engines and gas turbine aircraft engines as specified in head (5) of the entry in Group 3E relating to technology for aircraft and helicopters, and technology common to industrial gas turbine engines and marine gas turbine engines.
IL1399 Technology for the design of automatically controlled industrial systems used with software as specified in the entry in Group 3D relating thereto, whether or not such other equipment or systems are specified.
IL1425 Technology relating to floating docks, the following–
1 That portion of the design of a floating dock specially designed for use at remote locations relating to the incorporation of the following facilities–
a welding and pipe fitting repair shops;
b electrical and electronic repair workshops; and
c mechanical repair or metal working machine shops; and
2 The design, production and use of onboard floating dock facilities which permit the operation, maintenance and repair of nuclear reactors.
IL1460 Technology relating to aircraft and helicopters, the following–
1 Technology for aircraft and helicopter airframes, for aircraft propellers, and for aircraft and helicopter airframe, aircraft propeller, and helicopter rotor systems components, and specially designed software therefor, the following– a design technology using computer-aided aerodynamic analyses for integration of the fuselage, propulsion system and lifting and control surfaces to optimise aerodynamic performance throughout the flight regime of an aircraft; b technology for the design of active flight control systems, the following– i technology for configuration design for interconnecting multiple microelectronic processing elements (on-board computers) to achieve high-speed data transfer and high-speed data integration for control law implementation; ii technology for control law compensation for sensor location and dynamic airframe loads (compensation for sensor vibration environment and for variation of sensor location from centre of gravity); iii technology for electronic management of systems redundancy and data redundancy for fault detection, fault tolerance and fault isolation; iv technology for design of flight controls which permit in-flight reconfiguration of force and moment controls; c design technology for integration of flight control, navigation and propulsion control data into a flight management system for flight path optimisation; d design technology for protection of avionic and electrical sub-systems against electro-magnetic pulse (EMP) and electromagnetic interference (EMI) hazards from sources external to the aircraft, the following– i technology for design of shielding systems; ii technology for the configuration design of hardened electrical circuits and sub-systems; and iii determination of hardening criteria for the circuits and sub-systems specified in sub-head (d)(ii) above; e technology for the design, production and reconstruction of adhesively bonded airframe structural members designed to withstand operational temperatures in excess of 120°C; f technology for the design and production of propeller blades constructed wholly or partly of composite materials, and specially designed hubs therefor; g technology for the design and production of digital electronic synchrophasers specially designed for propellers, technology for the design of digital electronic controls for propellers and technology for the production of digital electronic controls for the propellers specified in sub-head (f) above; and h technology for the design and production of active laminar flow control lifting surfaces. i technology for the development of helicopter multi-axis fly-by-night or fly-by-wire controllers which combine the functions of at least two of the following into one controlling element– a Collective controls b Cyclic controls c Yaw controls j technology for the development of circulation controlled anti-torque or directional control systems for helicopters; k technology for the development of helicopter rotor blades incorporating variable geometry airfoils; l technology for the development of active control of helicopter blades and other surfaces used to generate aerodynamic forces and movements.
2 Technology for helicopter power transfer systems, except data resulting from helicopter power transfer system performance and installation design studies, and fabrication technology or overhaul and refurbishment technology for specific helicopter power transfer systems in civil use in bona fide civil helicopters for more than 8 years.
3 Technology for gas turbine engines and auxiliary power units (APUs) for use in aircraft or helicopters,
except data resulting from aircraft performance and installation design studies, and fabrication technology or overhaul and refurbishing technology for specific gas turbine aircraft engines or gas turbine powered aircraft APUs in civil use in bona fide civil aircraft or civil helicopters for more than 12 years.
IL1501 Technology, other than for installation, operation and maintenance, relating to the equipment specified in the exception to head 2(b) of the entry relating to navigation, direction finding, radar and airborne communication equipment.
IL1510 Technology or technical data associated with the design, manufacture or upgrading of an item not specified in IL1510 when such technology or technical data are also relevant to equipment specified in IL1510.
IL1519 Technology, other than for installation, operation or maintenance, relating to communication transmission equipment employing digital transmission techniques and designed for operation at a total bit rate at the highest multiplex point exceeding 2.1 Megabits per second.
IL1520 Technology, other than for installation, operation or maintenance, relating to radio relay communication equipment employing quadrature-amplitude-modulation (QAM) techniques.
IL1522 Technology, other than for installation, operation and maintenance, relating to uncooled, unsegmented mirrors with glass or dielectric substrates for use as end reflectors for laser resonators.
IL1537 Technology, other than for installation, operation and maintenance, relating to microwave assemblies, sub-assemblies or amplifiers (or combinations thereof) having all of the following characteristics–
1 Fixed tuned at the time of manufacture to operate only within the ITU satellite broadcasting band from 11.7 to 12.5 GHz;
2 Not capable of being retuned to a new frequency band by the user; and
3 Specially designed for use with or in civil television receivers.
IL1541 Technology for the design or production of cathode-ray tubes incorporating microchannel-plate electron multipliers.
IL1545 Technology unique to transistors based upon gallium arsenide.
IL1555 Technology for image intensifiers or converters incorporating fibre-optic face plates or microchannel-plate electron-multipliers, or electron tubes for cameras incorporating such intensifiers or converters.
IL1558 Technology relating to the equipment specified in the exception to the entry relating to electronic cathode-ray tubes, vacuum tubes and valves, specially designed for civil telecasting.
IL1560 Technology for the deisgn and production of tantalum capacitors rated for operation at ambient temperatures exceeding 125°C, except sintered electrolytic types having a casing made of epoxy resin or which are sealed or coated with epoxy resin.
IL1564 Technology relating to the export of wafer or chip design or processing information inherent in the manufacture of any class of “assembly”, “module”, “integrated circuit” or “circuit element”, specified in this schedule irrespective of any release of devices in any of these classes. This restriction also applies to technology embodied both in the equipment specified in IL1355 and in its use.
IL1565 Technology relating to electronic computers, the following–
1 Technology applicable to the–
a development, production or installation, operation and maintenance of electronic computers of any kind,
except
i technology which is unique to related equipment specified in sub-heads (b)(iv)(a), (iv)(b), (iv)(c), (iv)(e), (iv)(f), (iv)(l), (iv)(n), (iv)(p), or (iv)(q) of head (7) of the entry in Group 3G relating to computers and does not relate to equipment specified elsewhere in this Schedule; and
ii development, production or installation, operation and maintenance of equipment or systems specified in head (4) of the entry in Group 3G relating to computers.
2 Technology for the integration of–
a electronic computers or related equipment specified, other than as exceptions, in the entry in Group 3G relating to computers into other equipment or systems whether or not such other equipment or systems are so specified; or
b electronic equipment or related equipment not specified. other than as exceptions, in the entry in Group 3G relating to computers into other equipment or systems which are so specified.
IL1566 Technology applicable to the development, production or installation, operation and maintenance of software, whether or not such software is specified in this Schedule,
except the minimum technical information necessary for the use of software not so specified other than as an exception.
IL1567 Technology applicable to the development, production or installation, operation and maintenance of stored-programme-controlled communication switching equipment or systems, whether or not the equipment or systems are specified in the entry in Group 3G relating thereto,
except the minimum technical information necessary for the use of stored-programme-controlled communication switching equipment or systems not so specified, other than as exceptions.
IL1572 Technology, applicable to–
1 The development, production or use of recording or reproducing equipment specified in Group 3G
except
a technology which is unique to equipment specified in the exceptions in sub-heads 1(a), (b), 2 or 3 to IL1572;
b the minimum technology necessary for the use of equipment which may be exported under the provisions as specified in Group 3G relating to recording or reproducing equipment.
2 Technology for continuous coating of magnetic tape as specified in Group 3G relating to recording media.
except
a technology for the formulation of coating material;
b technology for the application of coating material to the backing.
3 Technology for the manufacture of flexible disk recording media as specified in Group 3G relating to recording media.
except
a technology for the formulation of coating material;
b technology for the application of coating material to the flexible backing;
4 Technology for the development or production of rigid disk recording media as specified in Group 3G relating to recording media.
IL1584 Technology, other than for maintenance, repair and operation, relating to oscilloscopes not specified in head (1) of the entry in Group 3G relating to oscilloscopes, which–
1 Use cathode-ray tubes specified in head (2) of the entry in Group 3F relating to cathode-ray tubes, or
2 Exceed an amplifier bandwidth of 200 MHz.
IL1587 Technology for quartz crystal elements or assemblies not specified in head (1) of the entry in Group 3G relating to quartz crystals.
IL1595 Technology or technical data associated with the design, manufacture or upgrading of equipment not specified in the entry in Group 3 relating to gravity meters, when such technology or technical data is also relevant to equipment specified in the entry in Group 3 relating to gravity meters.
IL1601 The process of inert gas and vacuum atomising for achieving sphericity and uniform size of particles in metal powders.
IL1602 Pyrolitic deposition technology and specially designed components therefor, the following–
1 Technology for producing pyrolitically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1,537 K (1,300°C) to 3,173 K (2,900°C) temperature range at pressures of 133.3 Pa to 19.995 kPa, including the composition of precursor gases, flow rates and process control schedules and parameters;
2 Specially designed nozzles for the processes specified in head (1) above.

SCHEDULE 2

  • The Export of Goods (Control) (Amendment) Order 1985 S.I. 1985/1085.
  • The Export of Goods (Control) (Amendment No. 2) Order 1985 S.I. 1985/1293.
  • The Export of Goods (Control) (Amendment No. 3) Order 1985 S.I. 1985/1294.
  • The Export of Goods (Control) (Amendment No. 4) Order 1986 S.I. 1986/82.
  • The Export of Goods (Control) (Amendment No. 5) Order 1986 S.I. 1986/540.
  • The Export of Goods (Control) (Amendment No. 6) Order 1986 S.I. 1986/1446.
  • The Export of Goods (Control) (Amendment No. 7) Order 1986 S.I. 1986/1934.
  • The Export of Goods (Control) (Amendment No. 8) Order 1987 S.I. 1987/215.
  • The Export of Goods (Control) (Amendment No. 9) Order 1987 S.I. 1987/271.
  • The Export of Goods (Control) (Amendment No. 10) Order 1987 S.I. 1987/1350.

Signed

Alan Clarke, — Minister for Trade, — Department of Trade and Industry — 26th November 1987.

Explanatory note

(This note is not part of the Order)

This Order revokes and replaces the Export of Goods (Control) Order 1985 and the subsequent amendments thereto. The changes (apart from minor and drafting changes) it effects are as follows–

1 Export control is– a lifted on fluorotantalates b reduced in scope on airborne, ground and marine navigation equipment, industrial transmitter and amplifier equipment, industrial telemetry and facsimile equipment, gyrotron electromagnets, magnetic materials, high-tensile aluminium alloys, fibrous and filamentary materials, electronic components. c extended in scope on ballistic protection materials, plutonium, nuclear reprocessing equipment, tritium production equipment, submersible systems, deep submergence vehicles, diode waveguide components, microwave antennae, electronic integrated circuits, polymeric materials. d amended in scope on deuterium, electronic measuring instruments, signal analysers, electronic components, polymeric materials, fluorocarbon compounds, compounds used in the synthesis of ultrafine polycrystalline silicon, resist material, certain ultra-pure metallo-organic and hydride compounds. e introduced on neptunium, nuclear separation materials, certain secondary (regenerative) cells, molten salt cells, amorphous alloy strips, certain chemicals; and on specific technologies, in respect of which the export of technological documents is controlled to certain destinations, relating to automatically controlled industrial systems, wafer or chip design or processed information inherent in the manufacture of assemblies, modules, integrated circuits or circuit elements, inert gas and vacuum atomising process, radio relay communications equipment, laser resonators, micro-wave assemblies, sub-assemblies or amplifiers, cathode-ray tubes, gallium arsenide-based transistors, image intensifiers, recording or reproducing equipment, oscilloscopes, quartz-crystal elements, gravity meters.

2 The descriptions of goods subject to export control have been amended in respect of induction furnaces, primary cells, electric arc equipment, electronic circuit assemblies.

3 Frequency changers have been transferred from Group 3C to Group 2B.

4 Copies of the British Standards referred to in these Regulations may be obtained from any of the sales outlets operated by the British Standards Institution (BSI), or by post from the BSI at 3 Linford Wood, Milton Keynes, MK14 6LE. Copies of the economic and control rules of the International Cocoa Agreement can be obtained from the International Cocoa Organisation, 22 Berners Street, London W7.

Footnotes

[^f00001]: 1939 c. 69.

[^f00002]: See S.I. 1970/1537.

[^f00003]: 1968 c. 59.

[^f00004]: See Council Regulation (EEC) No. 2658/87 O.J. No. L256, 7.9.87, p.1.

[^f00005]: O.J. No. L107, 22.4.87, p.1, amended by Regulation (EEC) 2823/87 (O.J. No. L270, 23.9.87, p.1).

[^f00006]: O.J. No. L307, 1.11.1982, p.36, amended by Commission Decisions 2149/84/ECSC (O.J. No. L202, 31.7.84, p.1) and 978/86/ECSC (O.J. No. L91, 7.4.86, p.49).

[^f00007]: O.J. No. L307, 1.11.1982, p.56, amended by Commission Regulations (EEC) 2150/84 (O.J. No. L202, 31.7.84, p.23) and 977/86 (O.J. No. L91, 7.4.86, p.1).

[^f00008]: O.J. No. L9, 10.1.1985, p.19, amended by Commission Regulation (EEC) No. 979/86 (O.J. No. L91, 7.4.86, p.96).

[^f00009]: Cmnd 9905.

[^f00010]: 1968 c. 27.

[^f00011]: S.I. 1981/155 (N.I. 2).

[^f00012]: Acts of Tynwald 1947 p.586.

[^f00013]: S.R. & O. 1931/413, 1937/525.

[^f00014]: O.J. No. L307, 1.11.82, p.27.

[^f00015]: O.J. No. L355, 31.12.85, p.155.

[^f00016]: O.J. No. L262, 13.9.86, p.12.

[^f00017]: O.J. No. L307, 1.11.82, p.3

[^f00018]: O.J. No. L355, 31.12.85, p.55. See also Commission communication 86/C44/05 (O.J. C44, 26.2.86, p.4).

[^f00019]: O.J. L262, 13.9.86, p.1.

[^f00020]: O.J. No. L9, 10.1.85, p.13, amended by Council Regulation (EEC) No. 3711/85 (O.J. No. L355, 31.12.85, p.100) and corrected by O.J. No. L115, 3.5.86, p.31.

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