The Export of Goods (Control) Order 1992

• (f) Accelerometer axis align stations.

7B102

Reflectometers specially designed to characterise mirrors, for laser gyros, having a measurement accuracy of 50ppm or less (better).

7B103

Specially designed production facilities for equipment specified in entry 7A117.

Materials

7C

None.

Software

7D

7D001

Software specially designed or modified for the development or production of goods specified in sub—categories 7A or 7B.

7D002

Source code for the use of any inertial navigation equipment or Attitude Heading Reference Systems (AHRS) (except: gimballed AHRS) including inertial equipment not specified in entries 7A003 or 7A004.

7D003

Other software, as follows:

• (a) Software specially designed or modified to improve the operational performance or reduce the navigational error of systems to the levels specified in entries 7A003 or 7A004;

• (b) Source code for hybrid integrated systems which improves the operational performance or reduces the navigational error of systems to the level specified in entry 7A003 by continuously combining inertial data with any of the following navigation data:

• (c) Source code for integrated avionics or mission systems which combine sensor data and employ knowledge—based expert systems;

• (d) Source code for the development of:

7D101

Software specially designed for the use of goods specified in entries 7A001 to 7A006, 7A101 to 7A106, 7A115, 7B002, 7B003, 7B102 or 7B103.

7D102

Integration software for the goods specified in entries 7A003 or 7A103.

Technology

7E

7E001

The export of goods specified in this entry is only prohibited to any destination in any country listed in Schedule 2.

7E002

The export of goods specified in this entry is only prohibited to any destination in any country listed in Schedule 2.

7E003

The export of goods specified in this entry is only prohibited to any destination in any country listed in Schedule 2.

except:

for maintenance technology directly associated with calibration, removal or replacement of damaged or unserviceable LRUs and (SRAs of a civil aircraft as described in Maintenance Level I or Maintenance Level II.

(see Technical Notes to entry 7B001)

7E004

The export of goods specified in heads a. and c. and sub—heads b.1., 2., 3., 4. and 6. of this entry is only prohibited to any destination in any country listed in Schedule 2.

7E101

Technology required for the use of goods specified in entries 7A001 to 7A006, 7A101 to 7A106, 7A115 to 7A117, 7B002, 7B003, 7B102, 7B103, 7D101 or 7D102.

7E102

Technology for protection of avionics and electrical subsystems against electromagnetic pulse (EMP) and electromagnetic interference (EMI) hazards, from external sources, as follows:

• (a) Design technology for shielding systems;

• (b) Design technology for the configuration of hardened electrical circuits and subsystems;

• (c) Design technology for the determination of hardening criteria for heads a. or b. of this entry.

7E104

Technology for the integration of the flight control, guidance, and propulsion data into a flight management system for optimization of rocket system trajectory.

Equipment, Assemblies and Components

8A

8A001

Submersible vehicles or surface vessels, as follows:

Note: For equipment for submersible vehicles, see:

Category 5 information security for encrypted communication equipment;

Category 6 for sensors;

Categories 7 and 8 for navigation equipment;

Category 8A for underwater equipment.

• (a) Manned, tethered submersible vehicles designed to operate at depths exceeding 1,000m;

• (b) Manned, untethered submersible vehicles:

• (c) Unmanned, tethered submersible vehicles designed to operate at depths exceeding 1,000m:

• (d) Unmanned, untethered submersible vehicles:

• (e) Ocean salvage systems with a lifting capacity exceeding 5MN for salvaging objects from depths exceeding 250m and having either of the following:

• (f) Surface—effect vehicles (fully skirted variety) with a maximum design speed, fully loaded, exceeding 30 knots in a significant wave height of 1·25m (Sea State 3) or more, a cushion pressure exceeding 3,830Pa, and a light—ship—to—full—load displacement ratio of less than 0·7;

• (g) Surface—effect vehicles (rigid sidewalls) with a maximum design speed, fully loaded, exceeding 40 knots in a significant wave height of 3·25m (Sea State 5) or more;

• (h) Hydrofoil vessels with active systems for automatically controlling foil systems, with a maximum design speed, fully loaded, of 40 knots or more in a significant wave height of 3·25m (Sea State 5) or more;

• (i) Small waterplane area vessels with:

8A002

Systems or equipment, as follows:

• (a) Systems or equipment, specially designed or modified for submersible vehicles, designed to operate at depths exceeding 1,000m, as follows:

• (b) Systems specially designed or modified for the automated control of the motion of equipment for submersible vehicles specified in entry 8A001 using navigation data and having closed loop servo—controls to:

• (c) Fibre optic hull penetrators or connectors;

• (d) Underwater vision systems, as follows:

• (a) Television systems (comprising camera, lights, monitoring and signal transmission equipment) having a limiting resolution when measured in air of more than 500 lines and specially designed or modified for remote operation with a submersible vehicle; or

• (b) Underwater television cameras having a limiting resolution when measured in air of more than 700 lines;

Technical Note: Limiting resolution in television is a measure of horizontal resolution usually expressed in terms of the maximum number of lines per picture height discriminated on a test chart, using Institution of Electrical and Electronic Engineers (IEEE) Standard 208/1960.

• (e) Photographic still cameras specially designed or modified for underwater use, having a film format of 35mm or larger, and:

• (f) Electronic imaging systems, specially designed or modified for underwater use, capable of storing digitally more than 50 exposed images;

• (g) Light systems, as follows, specially designed or modified for underwater use:

• (h) Robots specially designed for underwater use, controlled by using a dedicated stored programme computer:

• (i) Remotely controlled articulated manipulators specially designed or modified for use with submersible vehicles:

• (j) Air independent power systems, as follows, specially designed for underwater use:

• (k) Skirts, seals and fingers, as follows:

• (l) Lift fans rated at more than 400kW specially designed for surface effect vehicles specified in heads f. or g. of entry 8A001;

• (m) Fully submerged subcavitating or supercavitating hydrofoils specially designed for vessels specified in head h. of entry 8A001;

• (n) Active systems specially designed or modified to control automatically the sea—induced motion of vehicles or vessels specified in heads f., g., h. or i. of entry 8A001;

• (o)

• (o)

• (o)

• (p) Pumpjet propulsion systems with a power output exceeding 2·5MW using divergent nozzle and flow conditioning vane techniques to improve propulsive efficiency or reduce propulsion—generated underwater—radiated noise.

(For underwater communications systems, see Category 5 Telecommunications.)

8A990

The export of goods specified in this entry is only prohibited to any destination in Iran or Iraq.

8A991

The export of goods specified in this entry is only prohibited to any destination in Libya.

Test, Inspection and Production Equipment

8B

8B001

Water tunnels, having a background noise of less than 100dB (reference 1 micropascal, 1Hz) in the frequency range from 0 to 500Hz, designed for measuring acoustic fields generated by a hydro—flow around propulsion system models.

Materials

8C

8C001

Syntactic foam for underwater use:

• (a) Designed for marine depths exceeding 1,000m; and

• (b) With a density less than 561kg/m³.

Technical Note: Syntactic foam consists of hollow spheres of plastic or glass embedded in a resin matrix.

Software

8D

8D001

Software specially designed or modified for the development, production or use of goods specified in sub—categories 8A, 8B or 8C.

8D002

Specific software specially designed or modified for the development, production, repair, overhaul or refurbishing (re—machining) of propellers specially designed for underwater noise reduction.

Technology

8E

8E001

The export of goods specified in this entry is only prohibited to any destination in any country listed in Schedule 2.

8E002

The export of goods specified in this entry is only prohibited to any destination in any country listed in Schedule 2.

8E990

The export of goods specified in this entry is only prohibited to any destination in Iran or Iraq.

8E991

The export of goods specified in this entry is only prohibited to any destination in Libya.

Equipment, Assemblies and Components

9A

9A001

Aero gas turbine engines incorporating any of the technologies specified in head a. of entry 9E003, as follows[^f00051]:

• (a) Not certified for the specific civil aircraft for which they are intended;

• (b) Not certified for civil use by the aviation authorities in a relevant country;

Note: For the purposes of head b. of this entry, `relevant country' means an authority in Australia, Belgium, Canada, Denmark, Eire, France, Germany, Greece, Italy, Japan, Luxembourg, Netherlands, Norway, Portugal, Spain, Turkey, United Kingdom or United States of America.

• (c) Designed to cruise at speeds exceeding Mach 1·2 for more than thirty minutes.

9A002

Marine gas turbine engines with an ISO standard continuous power rating of 13,795kW or more and a specific fuel consumption of less than 0·243kg/kWh, and specially designed assemblies and components therefor.

9A003

Specially designed assemblies and components, incorporating any of the technologies specified in head a. of entry 9E003, for the following gas turbine engine propulsion systems:

• (a) Specified in entry 9A001; or

• (b) Whose design or production origins are either any country listed in Schedule 2 or are unknown to the manufacturer.

Note: This entry does not specify multiple domed combustors operating at average burner outlet temperatures equal to or less than 1,813K (1,540°C).

9A004

Space launch vehicles or spacecraft (not including their payloads)[^f00052].

(For products contained in spacecraft payloads, see the appropriate categories).

9A005

Liquid rocket propulsion systems containing any of the systems or components specified in entry 9A006[^f00053].

9A006

Systems or components, as follows[^f00054], specially designed for liquid rocket propulsion systems:

• (a) Cryogenic refrigerators, flightweight dewars, cryogenic heat pipes or cryogenic systems specially designed for use in space vehicles and capable of restricting cryogenic fluid losses to less than 30% per year;

• (b) Cryogenic containers or closed—cycle refrigeration systems capable of providing temperatures of 100K (−173°C) or less for aircraft capable of sustained flight at speeds exceeding Mach 3, launch vehicles or spacecraft;

• (c) Slush hydrogen storage or transfer systems;

• (d) High pressure (exceeding 17·5MPa) turbo pumps, pump components or their associated gas generator or expander cycle turbine drive systems;

• (e) High—pressure (exceeding 10·6MPa) thrust chambers and nozzles therefor;

• (f) Propellant storage systems using the principle of capillary containment or positive expulsion (i.e.,with flexible bladders).

9A007

Solid rocket propulsion systems with any of the following[^f00055]:

• (a)

• (b)

• (c) Any of the components specified in entry 9A008; or

• (d) Insulation and propellant bonding systems using direct—bonded motor designs to provide a strong mechanical bond or a barrier to chemical migration between the solid propellant and case insulation material.

Technical Note: For the purposes of head d. of this entry, a strong mechanical bond means bond strength equal to or more than propellant strength.

9A008

Components, as follows[^f00056], specially designed for solid rocket propulsion systems:

• (a) Insulation and propellant bonding systems using liners to provide a strong mechanical bond or a barrier to chemical migration between the solid propellant and case insulation material;

Technical Note: For the purposes of head a. of this entry, a strong mechanical bond means bond strength equal to or more than propellant strength.

• (b) Filament—wound composite motor cases exceeding 0·61m in diameter or having structural efficiency ratios (PV/W) exceeding 25km;

Technical Note: The structural efficiency ratio (PV/W) is the burst pressure (P) multiplied by the vessel volume (V) divided by the total pressure vessel weight (W).

• (c) Nozzles with thrust levels exceeding 45kN or nozzle throat erosion rates of less than 0·075mm/s;

• (d) Movable nozzle or secondary fluid injection thrust vector control systems capable of:

9A009

Hybrid rocket propulsion systems[^f00057] with:

• (a) Total impulse capacity exceeding 1·1MNs; or

• (b) Thrust levels exceeding 220kN in vacuum exit conditions.

9A010

Specially designed components or structures, for launch vehicles or launch vehicle propulsion systems, manufactured using metal matrix composite, organic composite, ceramic matrix or intermetallic reinforced materials specified in entries 1C007 or 1C010[^f00058].

9A011

Ramjet, scramjet or combined cycle engines and specially designed components therefor[^f00059].

9A101

Lightweight turbojet and turbofan engines (including turbocompound engines) that are small and fuel efficient and usable in missiles, other than those specified in entry 9A001.

9A104

Sounding rockets, capable of a range of at least 300km.

9A105

Liquid propellant rocket engines usable in missiles, other than those specified in entry 9A005, having a total impulse capacity of 1·1MNs or greater[^f00060].

9A106

Systems or components, other than those specified in entry 9A006, usable in missiles, as follows, specially designed for liquid rocket propulsion systems:

• (a) Rocket nozzles;

• (b) Thrust vector control sub—systems;

Technical Note: Examples of methods of achieving thrust vector control specified in head b. of this entry are:

• (c) Liquid and slurry propellant (including oxidiser) control systems, and specially designed components therefor, designed or modified to operate in vibration environments of more than 10grms between 20Hz and 2,000Hz.

Note: The only servo valves and pumps specified in head c. of this entry are as follows:

9A108

Components, other than those specified in entry 9A008, usable in missiles, as follows, specially designed for solid rocket propulsion systems:

• (a) Rocket motor cases, interior lining and insulation therefor;

Note: In this entry interior lining means suited for the bond interface between the solid propellant and the case or insulating liner. Usually a liquid polymer based dispersion of refractory or insulating materials, e.g., carbon filled hydroxy—terminated polybutadiene (HTPB) or other polymer with added curing agents sprayed or screeded over a case interior.

• (b) Rocket nozzles;

• (c) Thrust vector control sub—systems.

Technical Note: Examples of methods of achieving thrust vector control specified in head c. of this entry are:

9A109

Hybrid rocket motors, usable in missiles, other than those specified in entry 9A009, and specially designed components therefor[^f00061].

9A110

Composite structures, laminates and manufactures thereof, other than those specified in entry 9A010, including resin impregnated fibre prepregs and metal coated fibre preforms therefor, specially designed for use in the systems specified in entries 9A004 or 9A104 or the subsystems specified in entries 9A005, 9A007, 9A105, 9A106, 9A108 and 9A116, made either with organic matrix or metal matrix utilising fibre or filamentary reinforcements having a specific tensile strength greater than 7·62×10⁴ m and a specific modulus greater than 3·18×10⁶ m[^f00062].

9A111

Pulse jet engines, usable in missiles, and specially designed components therefor[^f00063].

9A115

Launch support equipment, designed or modified for systems specified in entries 9A004 or 9A104, as follows:

• (a) Apparatus and devices for handling, control, activation or launching;

• (b) Vehicles for transport, handling, control, activation or launching.

9A116

Reentry vehicles, usable in missiles, and equipment designed or modified therefor, as follows:

• (a) Heat shields and components therefor fabricated of ceramic or ablative materials;

• (b) Heat sinks and components therefor fabricated of light—weight, high heat capacity materials;

• (c) Electronic equipment specially designed for reentry vehicles.

9A117

Staging mechanisms, separation mechanisms, and interstages, usable in missiles.

9A118

Devices to regulate combustion usable in engines, which are usable in missiles, specified in entries 9A011 or 9A111.

9A119

Individual rocket stages, usable in missiles, other than those specified in entries 9A005, 9A007, 9A009, 9A105 or 9A109.

9A990

The export of goods specified in this entry is only prohibited to any destination in Libya, Iran, Iraq, Syria or South Africa.

9A991

Aircraft or steerable parachutes having a maximum all up weight of not more than 680kg.

9A992

The export of goods specified in this entry is only prohibited to any destination in Libya, Iran, Iraq, Syria or South Africa.

except:

Equipment and components specially designed for civil aircraft, where the aircraft type can be shown to have first flown before 1 January 1950.

Test, Inspection and Production Equipment

9B

9B001

Specially designed equipment, tooling or fixtures, as follows, for manufacturing or measuring gas turbine blades, vanes or tip shroud castings:

• (a) Automated equipment using non—mechanical methods for measuring airfoil wall thickness;

• (b) Tooling, fixtures or measuring equipment for the laser, water jet or ECM/EDM hole drilling processes specified in head c. of entry 9E003;

• (c) Directional solidification or single crystal casting equipment;

• (d) Ceramic cores or shells;

• (e) Ceramic core manufacturing equipment or tools;

• (f) Ceramic core leaching equipment;

• (g) Ceramic shell wax pattern preparation equipment;

• (h) Ceramic shell burn out or firing equipment.

9B002

On—line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for the development of gas turbine engines, assemblies or components incorporating technologies specified in head a. of entry 9E003.

9B003

Equipment specially designed for the production or test of gas turbine brush seals designed to operate at tip speeds exceeding 335m/s, and specially designed parts or accessories therefor.

9B004

Tools, dies or fixtures for the solid state joining of gas turbine superalloy or titanium components.

9B005

On—line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use with the following wind tunnels or devices:

• (a) Wind tunnels designed for speeds of Mach 1·2 or more;except:

those specially designed for educational purposes and having a test section size (measured laterally) of less than 250mm;

Technical Note: Test section size: the diameter of the circle, or the side of a square, or the longest side of a rectangle, at the largest test section location.

• (b) Devices for simulating flow—environments at speeds exceeding Mach 5, including hot—shot tunnels, plasma arc tunnels, shock tubes, shock tunnels, gas tunnels and light gas guns;

• (c) Wind tunnels or devices, other than two—dimensional sections, capable of simulating Reynolds number flows exceeding 25 × 10⁶.

9B006

Specially designed acoustic vibration test equipment capable of producing sound pressure levels of 160dB or more (referenced to 20 micropascals) with a rated output of 4kW or more at a test cell temperature exceeding 1,273.K (1,000°C), and specially designed transducers, strain gauges, accelerometers, thermocouples or quartz heaters therefor.

9B007

Equipment specially designed for inspecting the integrity of rocket motors using non—destructive test (NDT) techniques other than planar X—ray or basic physical or chemical analysis.

9B008

Transducers specially designed for the direct measurement of the wall skin friction of the test flow with a stagnation temperature exceeding 833K (560°C).

9B009

Tooling specially designed for producing turbine engine powder metallurgy rotor components capable of operating at stress levels of 60% of ultimate tensile strength (UTS) or more and metal temperatures of 873K (600°C) or more.

9B105

Wind tunnels for speeds of Mach 0·9 or more, usable for missiles and their subsystems.

9B106

Environmental chambers and anechoic chambers, as follows:

• (a) Environmental chambers capable of simulating the following flight conditions:

• (b) Anechoic chambers capable of simulating the following flight conditions:

9B115

Specially designed production equipment for the systems, sub—systems and components specified in entries 9A005 to 9A009, 9A011, 9A101, 9A105, 9A106, 9A108, 9A109, 9A111, 9A116 to 9A119.

9B116

Specially designed production facilities for the systems, sub—systems, and components specified in entries 9A004 to 9A009, 9A011, 9A101, 9A104 to 9A106, 9A108, 9A109, 9A111, 9A116 to 9A119.

9B117

Test benches and test stands for solid or liquid propellant rockets or rocket motors, having either of the following characteristics:

• (a) The capacity to handle more than 90kN of thrust; or

• (b) Capable of simultaneously measuring the three axial thrust components.

Materials

9C

None.

Software

9D

9D001

Software required for the development of goods or technology specified in sub—categories 9A, 9B or entry 9E003.

9D002

Software required for the production of goods specified in sub—categories 9A or 9B.

9D003

Software required for the use of full authority digital electronic engine controls (FADEC) for propulsion systems specified in sub—category 9A or equipment specified in sub—category 9B, as follows:

• (a) Software in digital electronic controls for propulsion systems, aerospace test facilities or air breathing aero—engine test facilities;

• (b) Fault—tolerant software used in FADEC systems for propulsion systems and associated test facilities.

9D004

Other software, as follows:

• (a) Software specially designed for vibration test equipment, other than that specified in entry 2D101, using real time digital controls with individual exciters (thrusters) with a maximum thrust exceeding 100kN;

• (b) 2D or 3D viscous software validated with wind tunnel or flight test data required for detailed engine flow modelling;

• (c) Software required for the development or production of real time full authority electronic test facilities for engines or components specified in sub—category 9A;

• (d) Software for testing aero gas turbine engines, assemblies or components, specially designed to collect, reduce and analyse data in real time, and capable of feedback control, including the dynamic adjustment of test articles or test conditions, as the test is in progress;

• (e) Software specially designed to control directional solidification or single crystal casting;

• (f) Software in source code, object code or machine code required for the use of active compensating systems for rotor blade tip clearance control.

Note: Head f. of this entry does not specify software embedded in non—specified equipment or required for maintenance activities associated with the calibration or repair or updates to the active compensating clearance control system.

9D101

Software specially designed for the use of goods specified in entries 9B105, 9B106, 9B116 or 9B117.

9D103

Software specially designed for modelling, simulation or design integration of missiles and their sub—systems.

Technology

9E

9E001

Technology required for the development of goods specified in head c. of entry 9A001, or entries 9A004 to 9A011, or sub—Categories 9B or 9D.

9E002

Technology required for the production of goods specified in head c. of entry 9A001, or entries 9A004 to 9A011 or sub—Category 9B.

9E003

The export of goods specified in this entry is only prohibited to any destination in any country listed in Schedule 2.

9E101

Technology required for the development or production of goods specified in entries 9A101, 9A104 to 9A106, 9A108 to 9A111 or 9A115 to 9A119.

9E102

Technology required for the use of goods specified in entries 9A004 to 9A011, 9A101, 9A104 to 9A106, 9A108 to 9A111, 9A115 to 9A119, 9B105, 9B106, 9B115, 9B116, 9B117, 9D101 or 9D103.

9E990

The export of goods specified in this entry is only prohibited to any destination in Libya, Iran, Iraq, Syria or South Africa.

9E991

Technology required for the development, production or use of goods specified in entry 9A991.

9E992

The export of goods specified in this entry is only prohibited to any destination in Libya, Iran, Iraq, Syria or South Africa.

SCHEDULE 2

Afghanistan

Albania

Armenia

Azerbaijan

Belarus

Bulgaria

China

Czech and Slovak Federal Republic

Estonia

Georgia

Kazakhstan

Kyrgyzstan

Latvia

Lithuania

Moldova

Mongolian People’s Republic

North Korea

Poland

Romania

Russian Federation

Socialist Republic of Vietnam

Tajikistan

Turkmenistan

Ukraine

Uzbekistan

SCHEDULE 3 — REVOCATIONS

The Export of Goods (Control) Order 1991[^f00065]

The Export of Goods (Control) (Amendment) Order 1992[^f00066]

The Export of Goods (Control) (Amendment No.2) Order 1992[^f00067]

The Export of Goods (Control) (Amendment No.3) Order 1992[^f00068]

Signed

Richard Needham — Minister for Trade — Department of Trade and Industry — 8th December 1992

Explanatory note

(This note is not part of the Order)

This Order revokes and replaces the Export of Goods (Control) Order 1991 (the “EGCO 1991”) and the amendments thereto. The changes (apart from minor drafting changes) it effects are as follows:—

The lists in Groups 2 and 3 of Part III (the “new lists”) are in a new format. The goods specified in these lists have been specified under international arrangements in COCOM and other groups, as goods which should be subject to export controls. The new lists have been largely prepared in consultations with technical experts from Member States of the European Communities with a view to the Member States operating export controls on commonly described nuclear and dual use goods. They have been prepared following the publication of a Commission proposal for a Regulation in relation to such goods (O.J.C253 30.9.92 p.13). A few entries have been included which have not, at the time of making of this Order, been considered by the said experts: 1 1C3521C3531C9901C9912B3523A9903E9905A9905E9908A9908A9918E9908E9919A9909A9919A9929E9909E9919E992. 2 Export control is relaxed in relation to certain dual use goods as follows: Ceramic base materials, fluorinated compounds and non—fluorinated polymeric components (see Category 1 of Group 3 of Schedule 1) (“Group 3”). Some machine tools, inspection machines, robots and bearings (see Category 2). DRAM’s (controls are lifted), many electronic components, some vacuum tubes, basic materials and semiconductor manufacturing equipment (see Category 3). Many types of computers and peripherals (see Category 4). Digital cellular telephone systems, data packet switches and multimode optical fibre systems (controls are lifted) (see Category 5). Some sensors and lenses (see Category 6). Some submersibles, hovercraft, pumpjet systems, underwater TV systems and some manipulators (see Category 8). Certified gas turbine engines for civil aircraft (controls are lifted), civil aircraft (see Category 9). 3 Export controls are extended to— a certain dual use goods for nuclear facilities and technology relating to them: those entries in Group 3 with numbers having a`2' in the third position e.g., 1C216 to all destinations b the following human and animal pathogens and chemical plant and biological equipment and technology relating to them to all destinations: entries in Group 3 numbered 1C351, 1C352, 1C353, 2B350, 2B351, 2B352, 1E001, 2E001 and 2E002. 4 a Compared to the list in Schedule 1 Part II of the EGCO 1991, the format and classification system for entries in the new lists has been changed. These changes are intended, where possible, to place controls on similar goods close to one another in the lists, and to enable changes to be made to the lists easily in future. b In the new lists goods are now specified by reference to a Category, sub—Category, Entry, head or sub—head. An example from the controls to illustrate this is 3A001a.4., where 3 is the Category, A is the sub—Category, 001 is the entry, a. is the head and 4 is the sub—head. c The PL entries from the EGCO 1991 have been moved, in some cases with modification, as follows: FromTo PL5003—Machine gun mountingsML1PL5005—Refuelling/disruption apparatusPL50063A990PL5009—Explosives and propellantsML81C1151C9911C2393A232PL5019—RadomesML4PL5024—Electrical pulsers3A229PL5026—Quartz crystals for ML4ML4PL6001—ThoriumA10PL6002—Fluorine1C990PL6003—Chlorine trifluoride1C238PL6005—Calcium1C227PL6006—Magnesium alloysDeletedPL6007—Gas centrifuge manufacture equipment1B2012B2042B2152B2282B229PL6008—Mass spectrometers3A233PL6009—Pressure gauges, corrosion resistant2B230PL6010—Process control equipment for irradiated lithium1B231PL6011—GraphiteA50PL6012—Deuterium compoundsA40PL6013—Blowers and compressors UF₆ corrosion resistantB10PL6014—Fluorinated hydrocarbon polymer powders, UF₆ resistantA70PL6015—UF₆ handling equipmentB20PL6016—Reprocessing plant equipmentB70PL7001—Aluminium alloys1C202a.PL7002—Maraging steel1C1161C216PL7003—Burst transmittersDeletedPL7004—EM proofed electronic equipment5A002d.PL7005—Internal grinding machineDeletedPL7006—Boron 101C225PL7007—Chemical Precursors1C350PL7008—Tropospheric scatter5A990PL7009—Vessels including ships8A9908A991PL7010—Aircraft and helicopters9A9909E990PL7011—Aircraft parts9A9929E992PL7012—Tantalum lined crucibles2A225PL7013—TransceiversDeletedPL7016—Microlights and steerable parachutes9A9919E991PL7017—Liquid and slurry propellant controls9A106c.PL7018—Pumps and servo valves for PL70179A106c.PL7019—Vacuum induction furnaces2B226PL7020—Telemetering and telecontrol equipment5A101PL7021—Laser radar—LIDAR6A008j.6A108a.PL7022—Solid state switches3A228PL7023—Cold cathode tubes3A228PL7025—Pyrolitic deposition technology9E1031B116PL7026—Ramjet engines, etc9A0119A111PL7027—Flow forming machines2B1152B215PL7028—Propellants for spacecraft1C115PL7029—Equipment for production in PL70281B115PL7030—Mixers for propellants1B115PL7031—Inert gas/vacuum atomising equipment1B002PL7032—Isostatic presses2B1042B204PL7033—CVD furnaces2B104PL7034—Graphites1C107PL7035—Tungsten particles1C117PL7036—Molybdenum particles1C117PL7037—Ground support equipment for missiles9A115PL7038—A—D PCBs or modulesML11PL7039—A—D I.C.s3A101a.PL7040—Test benches, stands for rocker motors9B117PL7041—Environmental/anechoic chambers9B106PL7042—Radiographic equipment3A101b.PL7043—Coatings for reduced observability1C101PL7044—Production equipment—rocket/jet engines9B1159B116PL7045—Technology for autoclaves1E103PL7046—Resaturated pyrolised materials1A102 d The structure of the new lists combined with the lifting of controls on many goods means that it is not practical to correlate and note all the controls with prefix IL in the EGCO 1991 list with the new lists. However, the changes have included moving certain of those controls into the Categories of Group 3 of the new list as follows: Category 1IL1310IL1357IL1561IL1610IL1631IL1672IL1675IL1710IL1733IL1746IL1754IL1763Category 2IL1001IL1088IL1091IL1099IL1312IL1362IL1370IL1371IL1388IL1389IL1391Category 3IL1205IL1355IL1529IL1531IL1533IL1537IL1558IL1560IL1564IL1568IL1572IL1586IL1757Category 4IL1565IL1566Category 5IL1353IL1502IL1516IL1517IL1519IL1520IL1522IL1526IL1527IL1529IL1531IL1533IL1537IL1565IL1566IL1567Category 6IL1353IL1370IL1389IL1501IL1502IL1510IL1522IL1526IL1548IL1555IL1556IL1571IL1574IL1585IL1595IL1757IL1767Category 7IL1485IL1501Category 8IL1319IL1363IL1416IL1417IL1418IL1759Category 9IL1080IL1086IL1361IL1362IL1401IL1431IL1460 e Group 2 of the new list has been renumbered and its contents restricted principally to items specially designed for use in the nuclear industry. Most nuclear items that have other uses are included in Group 3 of the new list as dual use industrial items. 5 The controls on the export of firearms (see Article 3) have been changed as a result of the Firearms Acts (Amendment) Regulations 1992 (1992/2823) and to implement Council Directive 91/477/EEC. 6 Persons who export under an Open General export Licence henceforth will, unless the licence states to the contrary, be required to register with the DTI before, or soon after doing so (see Article 8), and to keep records for a specified period. 7 Copies of the standards and recommendations referred to in this Order may be obtained from or through the British Standards Institution (BSI) at 3 Linford Wood, Milton Keynes, MK14 6LE, other than the ICAO and TCSEC standards mentioned at entries 5A001f., 5A002 and 6A008f., which may be obtained from the ICAO at 1000 Sherbrooke Street, Suite 400, Montreal, Canada H3A 2RZ, and the TCSEC, Technical Guidelines Division, National Computer Security Center, Ft. George G. Meade MD 20755–6000, U.S.A, respectively. 8 By way of assistance to the reader, and for convenience only, certain defined terms have been highlighted in Part III of Schedule 1 in bold type, and an index thereto, technical notes and certain cross—references have been included. These should not be treated as comprehensive. 9 Any particular goods may fall within more than one description in Schedule 1 to the Order. In such a case each prohibition (taking effect by such inclusion in that Schedule and the related provisions of article 2) applies to the export of the goods. This may mean that different entries prohibit the export of the goods to different countries.

Footnotes

[^f00001]: 1939 c. 69.

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

[^f00003]: OJ No. L256, 13.9.91, p.51.

[^f00004]: 1968 c. 27 as amended by the Firearms Acts (Amendment) Regulations 1992 (S.I. 1992/2823).

[^f00005]: 1968 c. 27, as amended by the Firearms (Amendment) Act 1988 c. 45.

[^f00006]: 1988 c. 45.

[^f00007]: S.I. 1981/155 (N.12), as amended.

[^f00008]: Acts of Tynwald 1947, p.586, as amended.

[^f00009]: Annex 1 to Commission Regulation (EEC) No. 2505/92 O.J. L267, 14.9.92, p1.

[^f00011]: See also PL 5029.

[^f00012]: See also entries 1A202, 9A010 and 9A110.

[^f00013]: See also entry 9A110.

[^f00014]: See also entries 1B101, 1B201.

[^f00015]: See also entry 1B201.

[^f00016]: See also entry 1C101.

[^f00017]: See also entry 1C202.

[^f00018]: See also entry 1C107.

[^f00019]: See also entry 1C210.

[^f00020]: See also entry 1C216.

[^f00021]: See also entry 1C991.

[^f00022]: See also ML7 of group 1 of part III of this schedule.

[^f00023]: See also ML7 of group 1 of part III of this schedule.

[^f00024]: O.J. L.16 23.1.92 p.19.

[^f00025]: See also ML7 of group 1 of part III of this schedule.

[^f00026]: See also entries 1C115, 1C239 or ML8 of group 1 of part III of this schedule.

[^f00027]: See also Entries 2B104 and 2B204.

[^f00028]: See also Entry 2B207.

[^f00029]: See also entry 2B215.

[^f00030]: See also Sub—category 3B.

[^f00031]: See also entry 9D004(a).

[^f00032]: See also entry 3A201.a.

[^f00033]: See also entry 3A201.b.

[^f00034]: See also entry 3A201.c.

[^f00035]: See also Group 1 of Part III of this Schedule.

[^f00036]: See also Group 1 of Part III of this Schedule.

[^f00037]: See also entry 4A101.

[^f00038]: See also entry 4A102.

[^f00039]: See also entry 6A102.

[^f00040]: See also Entry 6A203.

[^f00041]: See also entry 6A205.

[^f00042]: See also entry 6A107.

[^f00043]: See also entry 6A108.

[^f00044]: See also entry 7A101.

[^f00045]: See also entry 7A102.

[^f00046]: See also entry 7A103.

[^f00047]: See also entry 7A104.

[^f00048]: See also entry 7A105.

[^f00049]: See also entry 7A106.

[^f00050]: See also entry 7B102.

[^f00051]: See also entry 9A101.

[^f00052]: See also entry 9A104.

[^f00053]: See also entries 9A105 and 9A119.

[^f00054]: See also entry 9A106.

[^f00055]: See also entry 9A119.

[^f00056]: See also entry 9A108.

[^f00057]: See also entries 9A109 and 9A119.

[^f00058]: See also entries 1A002 and 9A110.

[^f00059]: See also entries 9A111 and 9A118.

[^f00060]: See also entry 9A119.

[^f00061]: See also entry 9A119.

[^f00062]: See also entry 1A002.

[^f00063]: See also entries 9A011 and 9A118.

[^f00064]: OJ L375, Vol23, 31.12.80, p.46.