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Chapter 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)

Original text. Later amendments are not shown.

IL1001Technology 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.

IL1080Technology, 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.

IL1372Technology 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.
IL1399Technology 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.
IL1425Technology 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.

IL1460Technology 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.

IL1501Technology, 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.
IL1510Technology 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.
IL1519Technology, 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.
IL1520Technology, other than for installation, operation or maintenance, relating to radio relay communication equipment employing quadrature-amplitude-modulation (QAM) techniques.
IL1522Technology, 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.
IL1537Technology, 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.

IL1541Technology for the design or production of cathode-ray tubes incorporating microchannel-plate electron multipliers.
IL1545Technology unique to transistors based upon gallium arsenide.
IL1555Technology 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.
IL1558Technology 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.
IL1560Technology 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.

IL1565Technology 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.

IL1572Technology, 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.

IL1584Technology, 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.

IL1587Technology for quartz crystal elements or assemblies not specified in head (1) of the entry in Group 3G relating to quartz crystals.
IL1595Technology 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.
IL1601The process of inert gas and vacuum atomising for achieving sphericity and uniform size of particles in metal powders.
IL1602Pyrolitic 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.