292 293 0C0010C001 "Natural uranium" or "depleted uranium" or thorium in the form of metal, alloy, chemical compound or concentrate and any other material containing one or more of the foregoing;0C0020C002 "Special fissile materials"294 0C0010C001 "Natural uranium" or "depleted uranium" or thorium in the form of metal, alloy, chemical compound or concentrate and any other material containing one or more of the foregoing;0C0020C002 "Special fissile materials"295 0C0010C001 "Natural uranium" or "depleted uranium" or thorium in the form of metal, alloy, chemical compound or concentrate and any other material containing one or more of the foregoing;296 0C0020C002 "Special fissile materials"1C012aa. Plutonium in any form with a plutonium isotopic assay of plutonium-238 of more than 50% by weight;297 0C0010C001 "Natural uranium" or "depleted uranium" or thorium in the form of metal, alloy, chemical compound or concentrate and any other material containing one or more of the foregoing;0C0020C002 "Special fissile materials"299 0A0010A001 "Nuclear reactors" and specially designed or prepared equipment and components therefor, as follows:a. Nuclear reactors;b. Metal vessels, or major shop-fabricated parts therefor, specially designed or prepared to contain the core of a "nuclear reactor", including the reactor vessel head for a reactor pressure vessel;c. Manipulative equipment specially designed or prepared for inserting or removing fuel in a "nuclear reactor";d. Control rods specially designed or prepared for the control of the fission process in a "nuclear reactor", support or suspension structures therefor, rod drive mechanisms and rod guide tubes;e. Pressure tubes specially designed or prepared to contain fuel elements and the primary coolant in a "nuclear reactor" at an operating pressure in excess of 5.1 MPa;f. Zirconium metal and alloys in the form of tubes or assemblies of tubes in which the ratio of hafnium to zirconium is less than 1:500 parts by weight, specially designed or prepared for use in a "nuclear reactor";g. Coolant pumps specially designed or prepared for circulating the primary coolant of "nuclear reactors";h. 'Nuclear reactor internals' specially designed or prepared for use in a "nuclear reactor", including support columns for the core, fuel channels, thermal shields, baffles, core grid plates, and diffuser plates;i. Heat exchangers (steam generators) specially designed or prepared for use in the primary coolant circuit of a "nuclear reactor";j. Neutron detection and measuring instruments specially designed or prepared for determining neutron flux levels within the core of a "nuclear reactor".

300 0C0030C003 Deuterium, heavy water (deuterium oxide) and other compounds of deuterium, and mixtures and solutions containing deuterium, in which the isotopic ratio of deuterium to hydrogen exceeds 1:5,000.301 0C0040C004 Graphite, nuclear grade, having a purity level of less than 5 parts per million 'boron equivalent' and with a density greater than 1.5 g/cm3. 305 0B0060B006 Plant for the reprocessing of irradiated "nuclear reactor" fuel elements, and specially designed or prepared equipment and components therefor.306 0B0050B005 Plant specially designed for the fabrication of "nuclear reactor" fuel elements and specially designed or prepared equipment therefor.1B2331B233 Lithium isotope separation facilities or plants, and equipment therefor, as follows:a. Facilities or plants for the separation of lithium isotopes;b. Equipment for the separation of lithium isotopes, as follows:1. Packed liquid-liquid exchange columns specially designed for lithium amalgams;2. Mercury or lithium amalgam pumps;3. Lithium amalgam electrolysis cells;4. Evaporators for concentrated lithium hydroxide solution.307 0B0010B001 Plant for the separation of isotopes of "natural uranium", "depleted uranium" and "special fissile materials", and specially designed or prepared equipment and components therefor, as follows:308 0B001cEquipment and components, specially designed or prepared for gaseous diffusion separation process, as follows:309 0B001bGas centrifuges and assemblies and components, specially designed or prepared for gas centrifuge separation process, as follows:310 0B001dEquipment and components, specially designed or prepared for aerodynamic separation process, as follows:311 0B001dEquipment and components, specially designed or prepared for aerodynamic separation process, as follows:312 0B001eEquipment and components, specially designed or prepared for chemical exchange separation process,as follows:0B001fEquipment and components, specially designed or prepared for ion-exchange separation process, as follows:313 0B001gEquipment and components, specially designed or prepared for atomic vapour laser isotope separation process (AVLIS), as follows:0B001hEquipment and components, specially designed or prepared for molecular laser isotope separation process (MLIS) or chemical reaction by isotope selective laser activation (CRISLA), as follows:314 0B001iEquipment and components, specially designed or prepared for plasma separation process, as follows:315 0B001jEquipment and components, specially designed or prepared for electromagnetic separation process, as follows:317 318 0B001b1313. Frequency changers (converters or inverters) specially designed or prepared to supply motor stators for gas centrifuge enrichment, having all of the following characteristics, and specially designed components therefor:319 0B001b13aa. Multiphase output of 600 to 2,000 Hz;320 0B001b13cc. Harmonic distortion of less than 2%; and321 0B001b13bb. Frequency control better than 0.1%;322 0B001b13dd. An efficiency greater than 80%;323 3A2253A225 Frequency changers or generators, other than those specified in 0B001.b.13., having all of the following characteristics:324 3A225aa. Multiphase output capable of providing a power of 40 W or greater;325 3A225bb. Capable of operating in the frequency range between 600 and 2000 Hz;326 3A225cc. Total harmonic distortion better (less) than 10%; and327 3A225dd. Frequency control better (less) than 0.1%.329 1C2401C240 Nickel powder and porous nickel metal, other than those specified in 0C005, as follows:a. Nickel powder having both of the following characteristics:1. A nickel purity content of 99.0% or greater by weight; and2. A mean particle size of less than 10 micrometres measured by American Society for Testing and Materials (ASTM) B330 standard;b. Porous nickel metal produced from materials specified in 1C240.a.330 0B0040B004 Plant for the production or concentration of heavy water, deuterium and deuterium compounds and specially designed or prepared equipment and components therefor, as follows:1B2291B229 Water-hydrogen sulphide exchange tray columns and 'internal contactors', as follows:331 0B004b0B004 Plant for the production or concentration of heavy water, deuterium and deuterium compounds and speciallydesigned or prepared equipment and components therefor, as followsb. Equipment and components, as follows:332 1B2291B229 Water-hydrogen sulphide exchange tray columns and 'internal contactors', as follows:3331B229aa. Water-hydrogen sulphide exchange tray columns, having all of the following characteristics:334 1B229a22 Constructed of carbon steel having an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; and335 1B229a11 Can operate at pressures of 2 MPa or greater;336 1B229b'Internal contactors for the water-hydrogen sulphide exchange tray columns specified in 1B229.a.337 1B229b'Internal contactors for the water-hydrogen sulphide exchange tray columns specified in 1B229.a.338 1B229bYTechnical Note: 'Internal contactors' of the columns are segmented trays which have an effective assembled diameter of 1.8 m or greater, are designed to facilitate countercurrent contacting and are constructed of stainless steels with a carbon content of 0.03% or less. These may be sieve trays, valve trays, bubble cap trays, or turbogrid trays.339 340 341 1B2281B228 Hydrogen-cryogenic distillation columns having all of the following characteristics:342 1B228cc. Constructed of either:1. Stainless steel of the 300 series with low sulphur content and with an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; or2. Equivalent materials which are both cryogenic and H2-compatible; and343 1B228dd. With internal diameters of 1 m or greater and effective lengths of 5 m or greater.344 1B228aa. Designed for operation with internal temperatures of 35 K (-238 ) or less;345 1B228bb. Designed for operation at an internal pressure of 0.5 to 5 MPa;346 1A2261A226 Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics:a. Made of phosphor bronze mesh chemically treated to improve wettability; andb. Designed to be used in vacuum distillation towers.347 1B2321B232 Turboexpanders or turboexpander-compressor sets having both of the following characteristics: a. Designed for operation with an outlet temperature of 35 K (-238 C) or less; and b. Designed for a throughput of hydrogen gas of 1000 kg/h or greater.348 1B2271B227 Ammonia synthesis converters or ammonia synthesis units, in which the synthesis gas (nitrogen and hydrogen) is withdrawn from an ammonia/hydrogen high-pressure exchange column and the synthesized ammonia is returned to said column.349 1B2301B230 Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH2/NH3), having all of the following characteristics:350 1B230aa. Airtight (i.e., hermetically sealed);351 1B230cc. Either of the following characteristics 1. For concentrated potassium amide solutions (1% or greater), an operating pressure of 1.5 to 60 MPa; or 2. For dilute potassium amide solutions (less than 1%), an operating pressure of20 to 60 MPa.352 1B230bb. A capacity greater than 8.5 m3/h; and354

0B0030B003 Plant for the conversion of uranium and equipment specially designed or prepared therefor, as follows:355 0B003aa. Systems for the conversion of uranium ore concentrates to UO3;356 0B003bb. Systems for the conversion of UO3 to UF6;0B003ee. Systems for the conversion of UF4 to UF6;357 0B003cc. Systems for the conversion of UO3 to UO2;0B003gg. Systems for the conversion of UF6 to UO2;358 0B003dd. Systems for the conversion of UO2 to UF4;0B003hh. Systems for the conversion of UF6 to UF4;359 0B003ff. Systems for the conversion of UF4 to uranium metal;360 0B003ii. Systems for the conversion of UO2 to UCl4.361

0B0070B007 Plant for the conversion of plutonium and equipment specially designed or prepared therefor, as follows:a. Systems for the conversion of plutonium nitrate to oxide;b. Systems for plutonium metal production.362 2B2092B209 Flow forming machines, spin forming machines capable of flow forming functions, other than those specified in 2B009 or 2B109, and mandrels, as follows:363 2B209aa. Machines having both of the following characteristics:1. Three or more rollers (active or guiding); and2. Which, according to the manufacturer's technical specification, can be equipped with "numerical control" units or a computer control;364 2B209bb. Rotor-forming mandrels designed to form cylindrical rotors of inside diameter between 75 mm and 400 mm.366 367 368 2B2012B201 Machine tools and any combination thereof, other than those specified in 2B001, as follows, for removing or cutting metals, ceramics or "composites", which, according to the manufacturers technical specification, can be equipped with electronic devices for simultaneous "contouring control" in two or more axes:2B001Machine tools and any combination thereof, for removing (or cutting) metals, ceramics or composites,which, according to the manufacturers technical specification, can be equipped with electronic devices fornumerical control, and specially designed components as follows:369 2B001aa. Machine tools for turning having all of the following:370 2B001a11. Positioning accuracy with all compensations available equal to or less (better) than 6 m according to ISO 230/2 (1988)(1)or national equivalents along any linear axis; and(1) Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of theMember State in which they are established.2B001a22. Two or more axes which can be coordinated simultaneously for contouring control;371 372 373 374 375 2B201aa. Machine tools for milling, having any of the following characteristics:376 2B201a11 Positioning accuracies with "all compensations available" equal to or less (better) than 6 m according to ISO 230/2 (1988)1 or national equivalents along any linear axis; or377 2B201a22 Two or more contouring rotary axes;378 2B001.b.2 379 2B201aXNote: 2B201.a. does not control milling machines having the following characteristics:380 2B201aXaa. X-axis travel greater than 2 m; and381 2B201aXbb. Overall positioning accuracy on the x-axis more (worse) than 30 m.382 2B201bb. Machine tools for grinding, having any of the following characteristics:383 2B201b11 Positioning accuracies with "all compensations available" equal to or less (better) than 4m according to ISO 230/2 (1988)1 or national equivalents along any linear axis; or384 2B201b22 Two or more contouring rotary axes.385 B001.c.2 386 2B201XNote: 2B201.b. does not control the following grinding machines:387 2B201bXa11. Limited to a maximum workpiece capacity of 150 mm outside diameter or length; and388 2B201bXa22. Axes limited to x, z and c;389 2B201bXNote: 2B201.b. does not control the following grinding machines:390 2B201bXbb. Jig grinders that do not have a z-axis or a w-axis with an overall positioning accuracy less (better) than 4 m according to ISO 230/2 (1988) or national equivalents.391 2B201bXbb. Jig grinders that do not have a z-axis or a w-axis with an overall positioning accuracy less (better) than 4 m according to ISO 230/2 (1988) or national equivalents.392 2B001dd. Electrical discharge machines (EDM) of the non-wire type which have two or more rotary axes which can be coordinated simultaneously for contouring control;393 2B201X1Note 1: 2B201 does not control special purpose machine tools limited to the manufacture of any of the following parts:3942B201X1aa. Gears;3952B201X1bb. Crankshafts or camshafts;3962B201X1cc. Tools or cutters;3972B201X1dd. Extruder worms.399 400 401 2B2062B206 Dimensional inspection machines, instruments or systems, other than those specified in 2B006, as follows:2B206X1Note 1: Machine tools that can be used as measuring machines are controlled if they meet or exceed the criteria specified for the machine tool function or the measuring machine function.402 2B206aa. Computer controlled or numerically controlled dimensional inspection machines having both of the following characteristics:403 2B206a11 Two or more axes; and404 2B206a22 A one-dimensional length "measurement uncertainty" equal to or less (better) than (1.25 + L/1000) ?m tested with a probe of an "accuracy" of less (better) than 0.2 m (L is the measured length in millimetres) (Ref.:VDI/VDE 2617 Parts 1 and 2);405 2B006bb. Linear and angular displacement measuring instruments, as follows:406 2B006b1aa. Non-contact type measuring systems with a "resolution" equal to or less (better) than 0.2 m within a measuring range up to 0.2 mm;407 2B006b1bb. Linear voltage differential transformer systems having all of the following characteristics:408 2B006b01b11. "Linearity" equal to or less (better) than 0.1% within a measuring range up to 5 mm; and409 2B006b01b22. Drift equal to or less (better) than 0.1% per day at a standard ambient test room temperature 1 K; or410 2B006b1cc. Measuring systems having all of the following:2B006b1XNote: 2B006.b.1. does not control measuring interferometer systems, with an automatic control system that is designed to use no feedback techniques, containing a "laser" to measure slide movement errors of machine-tools, dimensional inspection machines or similar equipment.411 2B006b1c11. Containing a "laser"; and412 '' 2B006b1c22. Maintaining, for at least 12 hours, at a temperature of 20 1 C, all of the following:a. A "resolution" over their full scale of 0.1 um or less (better); andb. Capable of achieving a measurement uncertainty, when compensated for therefractive index of air, equal to or less (better) than (0,2 + L/2 000) m (L is the measured length in mm); or413 2B006b22. Angular displacement measuring instruments having an "angular position deviation" equal to or less (better) than 0.00025;2B006b2XNote: 2B006.b.2. does not control optical instruments, such as autocollimators, using collimated light (e.g., laser light) to detect angular displacement of a mirror.414 2B206bb. Systems for simultaneous linear-angular inspection of hemishells, having both of the following characteristics:2B206Y1Technical Notes:1 The probe used in determining the measurement uncertainty of a dimensional inspection system shall be described in VDI/VDE 2617 parts 2, 3 and 4.415 2B206b11. "Measurement uncertainty" along any linear axis equal to or less (better) than 3.5m per 5 mm; and416 2B206b22. "Angular position deviation" equal to or less than 0.02.418 419 2B2262B226 Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows:2B226bb. Power supplies, with a specified power output of 5 kW or more, specially designed for furnaces specified in 2B226.a.2B226XNote: 2B226.a. does not control furnaces designed for the processing of semiconductor wafers.420 2B226a11. Capable of operation above 1,123 K (850C);421 2B226a22. Induction coils 600 mm or less in diameter; and422 2B226a33. Designed for power inputs of 5 kW or more;423 2B2272B227 Vacuum or other controlled atmosphere metallurgical melting and casting furnaces and related equipment as follows:a. Arc remelt and casting furnaces having both of the following characteristics:1. Consumable electrode capacities between 1,000 cm3 and 20,000 cm3; and2. Capable of operating with melting temperatures above 1,973 K (1,700oC);2B227cc. Computer control and monitoring systems specially configured for any of the furnaces specified in 2B227.a. or b.424 2B227bb. Electron beam melting furnaces and plasma atomization and melting furnaces, having both of the following characteristics:1. A power of 50 kW or greater; and2. Capable of operating with melting temperatures above 1,473 K (1,200).2B227cc. Computer control and monitoring systems specially configured for any of the furnaces specified in 2B227.a. or b.425 2B2042B204 "Isostatic presses", other than those specified in 2B004 or 2B104, and related equipment, as follows:2B204bb. Dies, moulds and controls, specially designed for "isostatic presses" specified in 2B204.a.426 2B204a11. Capable of achieving a maximum working pressure of 69 MPa or greater; and427 2B204a22. A chamber cavity with an inside diameter in excess of 152 mm;429 2B2072B207 "Robots", "end-effectors" and control units, other than those specified in 2B007, as follows:2B207bb. Control units specially designed for any of the "robots" or "end-effectors" specified in 2B207.a.430 ()(2B207aa. "Robots" or "end-effectors" specially designed to comply with national safety standards applicable to handling high explosives (for example, meeting electrical code ratings for high explosives);431 2B007cc. Specially designed or rated as radiation-hardened to withstand a total radiation dose greater than 5 x 10(3) Gy (silicon) without operational degradation; or433 2B1162B116 Vibration test systems, equipment and components therefor, as follows:434 2B116aa. Vibration test systems employing feedback or closed loop techniques and incorporating a digital controller, capable of vibrating a system at an acceleration equal to or greater than 10 g rms between 20 Hz and 2 kHz and imparting forces equal to or greater than 50 kN, measured 'bare table';435 436 437 438 2B116bb. Digital controllers, combined with specially designed vibration test software, with a real-time bandwidth greater than 5 kHz designed for use with vibration test systems specified in 2B116.a.;439 2B116cc. Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force equal to or greater than 50 kN, measured 'bare table', and usable in vibration test systems specified in 2B116.a.;440 2B116dd. Test piece support structures and electronic units designed to combine multiple shaker units in a system capable of providing an effective combined force equal to or greater than 50 kN, measured 'bare table', and usable in vibration systems specified in 2B116.a.441 442 1C202aa. Aluminium alloys having both of the following characteristics:1 'Capable of' an ultimate tensile strength of 460 MPa or more at 293 K (20C); and2 In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm;443 1C2101C210 'Fibrous or filamentary materials' or prepregs, other than those specified in 1C010.a., b. or e., as follows:1A2021A202 Composite structures, other than those specified in 1A002, in the form of tubes and having both of the following characteristics:444 1C210aa. Carbon or aramid 'fibrous or filamentary materials' having either of the following characteristics:445 1C210a11 A "specific modulus" of 12.7 x 10(6) m or greater; or446 1C210a22 A "specific tensile strength" of 235 x 10(3) m or greater;447 1C210bb. Glass 'fibrous or filamentary materials' having both of the following characteristics:448 1C210b11. A "specific modulus" of 3.18 x 10(6) m or greater; and449 1C210b22. A "specific tensile strength" of 76.2 x 10(3) m or greater;450 1C210cc. Thermoset resin impregnated continuous "yarns", "rovings", "tows" or "tapes" with a width of 15 mm or less (prepregs), made from carbon or glass 'fibrous or filamentary materials' specified in 1C210.a. or b.451 452 453 1A2021A202 Composite structures, other than those specified in 1A002, in the form of tubes and having both of the following characteristics:a. An inside diameter of between 75 mm and 400 mm; andb. Made with any of the "fibrous or filamentary materials" specified in 1C010.a. or b. or 1C210.a. or with carbon prepreg materials specified in 1C210.c.454 1C2161C216 Maraging steel, other than that specified in 1C116, 'capable of' an ultimate tensile strength of 2,050 MPa or more, at 293 K (20 C).1C216XNote: 1C216 does not control forms in which all linear dimensions are 75 mm or less.455 1C202bb. Titanium alloys having both of the following characteristics:1. 'Capable of' an ultimate tensile strength of 900 MPa or more at 293 K (20C); and2. In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm.457 1C2301C230 Beryllium metal, alloys containing more than 50% beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing.458 459 1C2291C229 Bismuth having both of the following characteristics:a. A purity of 99.99% or greater by weight; andb. Containing less than 10 parts per million by weight of silver460 1C2371C237 Radium-226 (226Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium-226, manufactures therof, and products or devices containing any of the foregoing.1C237XNote: 1C237 does not control the following:a. Medical applicators;b. A product or device containing less than 0.37 GBq (10 millicuries) of radium-226.461 1C2361C236 Alpha-emitting radionuclides having an alpha half-life of 10 days or greater but less than 200 years, in the following forms:a.Elemental;b.Compounds having a total alpha activity of 37 GBq/kg (1 Ci/kg) or greater;c. Mixtures having a total alpha activity of 37 GBq/kg (1 Ci/kg) or greater;1C236XNote: 1C236 does not control a product or device containing less than 3.7 GBq (100 millicuries) of alpha activity.463 1C2251C225 Boron enriched in the boron-10 (10B) isotope to greater than its natural isotopic abundance, as follows: elemental boron, compounds, mixtures containing boron, manufactures thereof, waste or scrap of any of the foregoing.464 465 1C2271C227 Calcium having both of the following characteristics:466 1C227aa. Containing less than 1,000 parts per million by weight of metallic impurities other than magnesium; and467 1C227bb. Containing less than 10 parts per million by weight of boron.468 1C2381C238 Chlorine trifluoride (ClF3).469 1C2281C228 Magnesium having both of the following characteristics:470 1C228aa. Containing less than 200 parts per million by weight of metallic impurities other than calcium; and471 1C228bb. Containing less than 10 parts per million by weight of boron.472 2A2252A225 Crucibles made of materials resistant to liquid actinide metals, as follows:473 2A225aa. Crucibles having both of the following characteristics:1. A volume of between 150 cm3 and 8,000 cm3; and2. Made of or coated with any of the following materials, having a purity of 98% or greater by weight:474 2A225a2aa. Calcium fluoride (CaF2);475 2A225a2bb. Calcium zirconate (metazirconate) (CaZrO3);476 2A225a2cc. Cerium sulphide (Ce2S3);477 2A225a2dd. Erbium oxide (erbia) (Er2O3);478 2A225a2ee. Hafnium oxide (hafnia) (HfO2);479 2A225a2ff. Magnesium oxide (MgO);480 2A225a2gg. Nitrided niobium-titanium-tungsten alloy (approximately 50% Nb, 30% Ti, 20% W);481 2A225a2hh. Yttrium oxide (yttria) (Y2O3); or482 2A225a2ii. Zirconium oxide (zirconia) (ZrO2);483 2A225bb. Crucibles having both of the following characteristics:1. A volume of between 50 cm3 and 2,000 cm3; and2. Made of or lined with tantalum, having a purity of 99.9% or greater by weight;484 2A225cc. Crucibles having all of the following characteristics:1. A volume of between 50 cm3 and 2,000 cm3;2. Made of or lined with tantalum, having a purity of 98% or greater by weight; and3. Coated with tantalum carbide, nitride, boride, or any combination thereof.486 1C2311C231 Hafnium metal, alloys containing more than 60% hafnium by weight, hafnium compounds containing more than 60% hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing.487 1C2331C233 Lithium enriched in the lithium-6 (6Li) isotope to greater than its natural isotopic abundance, and products or devices containing enriched lithium, as follows: elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.1C233XNote: 1C233 does not control thermoluminescent dosimeters.488 1C2261C226 Tungsten, tungsten carbide, and alloys containing more than 90% tungsten by weight, having both of the following characteristics: a. In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 mm and 300 mm; and b. A mass greater than 20 kg.1C226XNote: 1C226 does not control manufactures specially designed as weights or gamma-ray collimators.489 1C2341C234 Zirconium with a hafnium content of less than 1 part hafnium to 500 parts zirconium by weight, as follows: metal, alloys containing more than 50% zirconium by weight, compounds, manufactures thereof, waste or scrap of any of the foregoing.1C234XNote: 1C234 does not control zirconium in the form of foil having a thickness of 0.10 mm or less.490 1B2251B225 Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour.491 2B2282B228 Rotor fabrication or assembly equipment, rotor straightening equipment, bellows-forming mandrels and dies, as follows:492 2B228aa. Rotor assembly equipment for assembly of gas centrifuge rotor tube sections, baffles, and end caps;493 2B228bb. Rotor straightening equipment for alignment of gas centrifuge rotor tube sections to a common axis;494 2B228cc. Bellows-forming mandrels and dies for producing single-convolution bellows.2B228cY4Technical Note: In 2B228.c. the bellows have all of the following characteristics: 4. Made of high-strength aluminium alloys, maraging steel or high strength "fibrous or filamentary materials".495 2B228cY11 Inside diameter between 75 mm and 400 mm;496 2B228cY22 Length equal to or greater than 12.7 mm;497 2B228cY33 Single convolution depth greater than 2 mm; and498 2B2192B219 Centrifugal multiplane balancing machines, fixed or portable, horizontal or vertical, as follows:499 2B219aa. Centrifugal balancing machines designed for balancing flexible rotors having a length of 600 mm or more and having all of the following characteristics:500 2B219a11. Swing or journal diameter greater than 75 mm;501 2B219a22. Mass capability of from 0.9 to 23 kg ; and502 2B219a33. Capable of balancing speed of revolution greater than 5,000 r.p.m.;503 2B219bb. Centrifugal balancing machines designed for balancing hollow cylindrical rotor components and having all of the following characteristics:504 2B219b11. Journal diameter greater than 75 mm;505 2B219b22. Mass capability of from 0.9 to 23 kg;506 2B219b33. Capable of balancing to a residual imbalance equal to or less than 0.01 kg x mm/kg per plane; and507 2B219b44. Belt drive type.508 1B2011B201 Filament winding machines, other than those specified in 1B001 or 1B101, and related equipment, as follows: a. Filament winding machines having all of the following characteristics: b. Coordinating and programming controls for the filament winding machines specified in 1B201.a.; c. Precision mandrels for the filament winding machines specified in 1B201.a.509 1B201a11. Having motions for positioning, wrapping, and winding fibres coordinated and programmed in two or more axes;510 1B201a33. Capable of winding cylindrical rotors of diameter between 75 and 400 mm and lengths of 600 mm or greater;512 6A2056A205 "Lasers", "laser" amplifiers and oscillators, other than those specified in 0B001.g.5., 0B001.h.6. and 6A005; as follows:513 6A005bb. Non-tunable pulsed lasers having any of the following: 2. Output wavelength of 150 nm or more but not exceeding 520 nm and any of the following: a. Output energy exceeding 1,5 J per pulse and peak power exceeding 30 W; or b. Average output power exceeding 30 W; 3.utput wavelength exceeding 520 nm but not exceeding 540 nm and any of the following: a. Single transverse mode output and any of the following: 1. Output energy exceeding 1,5 J per pulse and peak power exceeding 50 W; or 2. Average output power exceeding 50 W; or b. Multiple transverse mode output and any of the following: 1. Output energy exceeding 1,5 J per pulse and peak power exceeding 150 W; or 2. Average output power exceeding 150 W; 4. Output wavelength exceeding 540 nm but not exceeding 800 nm and any of the following: a. Output energy exceeding 1,5 J per pulse and peak power exceeding 30 W; or b. Average output power exceeding 30 W; 514 6A205aa. Argon ion "lasers" having both of the following characteristics:1 Operating at wavelengths between 400 nm and 515 nm; and2 An average output power greater than 40 W;515 6A205dd. Pulsed carbon dioxide "lasers" having all of the following characteristics:6A205d11 Operating at wave lengths between 9,000 nm and 11,000 nm;516 6A205d22 A repetition rate greater than 250 Hz;517 6A205d33 An average output power greater than 500 W; and518 6A205d44 Pulse width of less than 200 ns;519 6A005d4cd. Other lasers, not specified in 6A005.a., 6A005.b. or 6A005.c. as follows: 4. Excimer lasers having any of the following: c. Output wavelength exceeding 190 nm but not exceeding 360 nm and any of the following: 1. Output energy exceeding 10 J per pulse; or 2. Average output power exceeding 500 W; or 522 6A205ee. Para-hydrogen Raman shifters designed to operate at 16 micrometre output wavelength and at a repetition rate greater than 250 Hz;523 6A005c2c. Tunable lasers having any of the following:Note: 6A005.c. includes titaniumsapphire (Ti: Al2O3), thulium-YAG (Tm: YAG), thulium-YSGG (Tm: YSGG),alexandrite (Cr: BeAl2O4), colour centre lasers, dye lasers, and liquid lasers. 2. Output wavelength of 600 nm or more but not exceeding 1 400 nm, and any of the following: a. Output energy exceeding 1 J per pulse and peak power exceeding 20 W; or b. Average or CW output power exceeding 20 W; or 527 6A205ff. Neodymium-doped (other than glass) "lasers" with an output wavelength between 1000 and 1100 nm having either of the following528 6A205f11. Pulse-excited and Q-switched with a pulse duration equal to or more than 1 ns, and having either of the following:529 6A205f1aa. A single?transverse mode output with an average output power greater than 40W; or530 6A205f1bb. A multiple-transverse mode output having an average power greater than 50 W; or531 6A205f22. Incorporating frequency doubling to give an output wavelength between 500 and 550 nm with an average output power of more than 40 W.532 6A205bb. Tunable pulsed single-mode dye laser oscillators having all of the following characteristics:6A205b11 Operating at wavelengths between 300 nm and 800 nm;6A205cc. Tunable pulsed dye laser amplifiers and oscillators, having all of the following characteristics:6A205c11 Operating at wavelengths between 300 nm and 800 nm;533 6A205bb. Tunable pulsed single-mode dye laser oscillators having all of the following characteristics:534 6A205b33. A repetition rate greater than 1 kHz; and535 6A205b22. An average output power greater than 1 W;536 6A205b44. Pulse width less than 100 ns;537 6A205cc. Tunable pulsed dye laser amplifiers and oscillators, having all of the following characteristics:538 6A205c33. A repetition rate greater than 1 kHz; and539 6A205c22. An average output power greater than 30 W;540 6A205c44. Pulse width less than 100 ns;542 3A2333A233 Mass spectrometers, other than those specified in 0B002.g., capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor:543 3A233aa. Inductively coupled plasma mass spectrometers (ICP/MS);544 3A233bb. Glow discharge mass spectrometers (GDMS);545 3A233cc. Thermal ionization mass spectrometers (TIMS);546 3A233dd. Electron bombardment mass spectrometers which have a source chamber constructed from, lined with or plated with materials resistant to UF6;547 3A233ee. Molecular beam mass spectrometers having either of the following characteristics:548 3A233e11. A source chamber constructed from, lined with or plated with stainless steel or molybdenum and equipped with a cold trap capable of cooling to 193 K (-80oC) or less; or549 3A233e22. A source chamber constructed from, lined with or plated with materials resistant to UF6;550 3A233ff. Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides.551 0B002gg. UF6 mass spectrometers/ion sources specially designed or prepared for taking on-line samples of feed, product or tails from UF6 gas streams and having all of the following characteristics:552 0B002g11. Unit resolution for mass of more than 320 amu;553 0B002g22 Ion sources constructed of or lined with nichrome or monel, or nickel plated;554 0B002g33 Electron bombardment ionisation sources; and555 0B002g44 Collector system suitable for isotopic analysis.556 0B002gg. UF6 mass spectrometers/ion sources specially designed or prepared for taking on-line samples of feed, product or tails from UF6 gas streams and having all of the following characteristics:558 559 2B230aa. Pressure sensing elements made of or protected by aluminium, aluminium alloy, nickel or nickel alloy with more than 60% nickel by weight; and560 2B230b11. A full scale of less than 13 kPa and an 'accuracy' of better than 1% of full-scale; or561 2B230b22. A full scale of 13 kPa or greater and an 'accuracy' of better than 130 Pa.562 2A2262A226 Valves having all of the following characteristics:a. A 'nominal size' of 5 mm or greater;b. Having a bellows seal; andc. Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60% nickel by weight.564 3A201bb. Superconducting solenoidal electromagnets having all of the following characteristics:3A201bXNote: 3A201.b. does not control magnets specially designed for and exported 'as parts of' medical nuclear magnetic resonance (NMR) imaging systems. The phrase 'as part of' does not necessarily mean physical part in the same shipment; separate shipments from different sources are allowed, provided the related export documents clearly specify that the shipments are dispatched 'as part of' the imaging systems.565 3A201b11 Capable of creating magnetic fields greater than 2 T;566 3A201b22 A ratio of length to inner diameter greater than 2;567 3A201b33 Inner diameter greater than 300 mm; and568 3A201b44 Magnetic field uniform to better than 1% over the central 50% of the inner volume;570 2B2312B231 Vacuum pumps having all of the following characteristics:a. Input throat size equal to or greater than 380 mm;b. Pumping speed equal to or greater than 15 m3/s; andc. Capable of producing an ultimate vacuum better than 13 mPa.571 3A2263A226 High-power direct current power supplies, other than those specified in 0B001.j.6., having both of the following characteristics:3A2273A227 High-voltage direct current power supplies, other than those specified in 0B001.j.5., having both of the following characteristics:572 3A226aa. Capable of continuously producing, over a time period of 8 hours, 100 V or greater with current output of 500 A or greater; and3A226bb. Current or voltage stability better than 0.1% over a time period of 8 hours.573 3A227aa. Capable of continuously producing, over a time period of 8 hours, 20 kV or greater with current output of 1 A or greater; and3A227bb. Current or voltage stability better than 0.1% over a time period of 8 hours.574 3A201cc. Flash X-ray generators or pulsed electron accelerators having either of the following sets of characteristics:3A201cXNote: 3A201.c. does not control accelerators that are component parts of devices designed for purposes other than electron beam or X-ray radiation (electron microscopy, for example) nor those designed for medical purposes:575 3A201c1c.1. a. An accelerator peak electron energy of 500 keV or greater but less than 25 MeV; and b. With a 'figure of merit' (K) of 0.25 or greater; or

Technical Notes: 1. The figure of merit K is defined as: K=1.710(3)V(2.65)Q V is the peak electron energy in million electron volts. If the accelerator beam pulse duration is less than or equal to 1 s, then Q is the total accelerated charge inCoulombs. If the accelerator beam pulse duration is greater than 1 s, then Q is the maximum acceleratedcharge in 1 s. Q equals the integral of i with respect to t, over the lesser of 1 s or the time duration of the beam pulse(Q = idt), where i is beam current in amperes and t is time in seconds.576 ''577 ''578 3A201c22. Flash X-ray generators or pulsed electron accelerators having either of the following sets of characteristics:a. An accelerator peak electron energy of 25 MeV or greater; and b. A 'peak power' greater than 50 MW.580 2B2322B232 Multistage light gas guns or other high-velocity gun systems (coil, electromagnetic, and electrothermal types, and other advanced systems) capable of accelerating projectiles to 2 km/s or greater.581 582 6A203aa. Mechanical rotating mirror cameras, as follows, and specially designed components therefor:583 6A203a22. Streak cameras with writing speeds greater than 0.5 mm per microsecond;584 6A203a11. Framing cameras with recording rates greater than 225,000 frames per second;585 ''6A203bb. Electronic streak cameras, electronic framing cameras, tubes and devices, as follows:586 6A203b11 Electronic streak cameras capable of 50 ns or less time resolution;6A203b22 Streak tubes for cameras specified in 6A203.b.1.;587 6A203b33 Electronic (or electronically shuttered) framing cameras capable of 50 ns or less frame exposure time;588 6A203b4dd. Other framing tubes and solid-state imaging devices having a fast-image gating time of less than 50 ns specially designed for cameras specified in 6A203.b.3.;589 6A203b44 Framing tubes and solid-state imaging devices for use with cameras specified in 6A203.b.3., as follows:590 6A203b4aa. Proximity focused image intensifier tubes having the photocathode deposited on a transparent conductive coating to decrease photocathode sheet resistance;591 6A203b4bb. Gate silicon intensifier target (SIT) videcon tubes, where a fast system allows gating the photoelectrons from the photocathode before they impinge on the SIT plate;592 6A203b4cc. Kerr or Pockels cell electro-optical shuttering;594 595

6A2256A225 Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 microseconds.598 6A2266A226 Pressure sensors, as follows: a. Manganin gauges for pressures greater than 10 GPa; b. Quartz pressure transducers for pressures greater than 10 GPa.600 3A228aa. Cold-cathode tubes, whether gas filled or not, operating similarly to a spark gap, having all of the following characteristics:3A228a11. Containing three or more electrodes;601 3A228a22. Anode peak voltage rating of 2.5 kV or more;602 3A228a33. Anode peak current rating of 100 A or more; and603 3A228a44. Anode delay time of 10 s or less;605 3A228bb. Triggered spark-gaps having both of the following characteristics: 1. An anode delay time of 15 s or less; and 2. Rated for a peak current of 500 A or more;606 3A228cc. Modules or assemblies with a fast switching function, other than those specified in 3A001.g., having all of the following characteristics:607 3A228c11. Anode peak voltage rating greater than 2 kV;608 3A228c22. Anode peak current rating of 500 A or more; and609 3A228c33. Turn-on time of 1 us or less.611 3A201aa. Capacitors having either of the following sets of characteristics:612 3A201a1a1. a. Voltage rating greater than 1.4 kV;613 3A201a1bb. Energy storage greater than 10 J;614 3A201a1cc. Capacitance greater than 0.5 F; and615 3A201a1dd. Series inductance less than 50 nH; or616 3A201a2a2. a. Voltage rating greater than 750 V;617 3A201a2bb. Capacitance greater than 0.25 F; and618 3A201a2cc. Series inductance less than 10 nH;620 3A2293A229 High-current pulse generators as follows:3A2303A230 High-speed pulse generators having both of the following characteristics:621 3A229bb. Modular electrical pulse generators (pulsers) having all of the following characteristics:3A229bXNote: 3A229.b. includes xenon flash-lamp drivers.622 3A229b33. Capable of delivering their energy in less than 15s;623 3A229b44. Having an output greater than 100 A;624 3A229b55. Having a 'rise time' of less than 10 us into loads of less than 40 ohms;625 3A229b66. No dimension greater than 254 mm;626 3A229b77. Weight less than 25 kg; and627 3A229b88. Specified for use over an extended temperature range 223 K (-50 ) to 373 K (100 ) or specified as suitable for aerospace applications. 3A230High-speed pulse generators having both of the following characteristics:a. Output voltage greater than 6 V into a resistive load of less than 55 ohms, andb. 'Pulse transition time' less than 500 ps.630 631 6A2026A202 Photomultiplier tubes having both of the following characteristics:a. Photocathode area of greater than 20 cm2; andb. Anode pulse rise time of less than 1 ns.632 3A2313A231 Neutron generator systems, including tubes, having both of the following characteristics:a. Designed for operation without an external vacuum system; andb. Utilizing electrostatic acceleration to induce a tritium-deuterium nuclear reaction.633 2B2252B225 Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells, having either of the following characteristics:a. A capability of penetrating 0.6 m or more of hot cell wall (through-the-wall operation); orb. A capability of bridging over the top of a hot cell wall with a thickness of 0.6 m or more (over-the-wall operation).634 1A2271A227 High-density (lead glass or other) radiation shielding windows, having all of the following characteristics, and specially designed frames therefor:635 1A227aa. A 'cold area' greater than 0.09 m2;636 1A227bb. A density greater than 3 g/cm3; and637 1A227cc. A thickness of 100 mm or greater.639 6A203cc. Radiation-hardened TV cameras, or lenses therefor, specially designed or rated as radiation hardened to withstand a total radiation dose greater than 50 x 103 Gy(silicon) (5 x 106 rad (silicon)) without operational degradation.640 1C2351C235 Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1000, and products or devices containing any of the foregoing.1C235XNote: 1C235 does not control a product or device containing less than 1.48 x 10(3) GBq (40 Ci) of tritium.641 1B2311B231 Tritium facilities or plants, and equipment therefor, as follows:642 1B231aa. Facilities or plants for the production, recovery, extraction, concentration, or handling of tritium;643 1B231bb. Equipment for tritium facilities or plants, as follows:644 1B231b11. Hydrogen or helium refrigeration units capable of cooling to 23 K (-250) or less, with heat removal capacity greater than 150 W;645 1B231b22. Hydrogen isotope storage or purification systems using metal hydrides as the storage or purification medium.646 1A2251A225 Platinized catalysts specially designed or prepared for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water.647 1C2321C232 Helium-3 (3He), mixtures containing helium-3, and products or devices containing any of the foregoing.1C232XNote: 1C232 does not control a product or device containing less than 1 g of helium-3.648 649 1C3501C350 Chemicals, which may be used as precursors for toxic chemical agents, as follows, and "chemical mixtures" containing one or more thereof:650 1C350 1010. 3-Hydroxy-1-methylpiperidine (3554-74-3);651 1C350 1414. Potassium fluoride (7789-23-3);652 1C350 1515. 2-Chloroethanol (107-07-3);653 1C350 1616. Dimethylamine (124-40-3);654 1C350 2020. Dimethylamine hydrochloride (506-59-2);655 1C350 2424. Hydrogen fluoride (7664-39-3);656 1C350 2525. Methyl benzilate (76-89-1);657 1C350 3737. 3-Quinuclidone (3731-38-2);658 1C350 3939. Pinacolone (75-97-8);659 1C350 4040. Potassium cyanide (151-50-8);660 1C350 4141. Potassium bifluoride (7789-29-9);661 1C350 4242. Ammonium hydrogen fluoride or ammonium bifluoride (1341-49-7);662 1C350 4444. Sodium bifluoride (1333-83-1);663 1C350 4343. Sodium fluoride (7681-49-4);664 1C350 4545. Sodium cyanide (143-33-9);665 1C350 4747. Phosphorus pentasulphide (1314-80-3);666 1C350 4848. Di-isopropylamine (108-18-9);667 1C350 4949. Diethylaminoethanol (100-37-8);668 1C350 5050. Sodium sulphide (1313-82-2);669 1C350 5353. Triethanolamine hydrochloride (637-39-8);670 1C350 5858. Triisopropyl phosphite (116-17-6);671 1C350 6060. O,O-Diethyl phosphorothioate (2465-65-8);672 1C350 6161. O,O-Diethyl phosphorodithioate (298-06-6);673 1C350 6262. Sodium hexafluorosilicate (16893-85-9);675 1C4501C450 Toxic chemicals and toxic chemical precursors, as follows, and "chemical mixtures" containing one or more thereof:676 []1C450a11. Amiton: O,O-Diethyl S-[2-(diethylamino)ethyl] phosphorothiolate (78-53-5) and corresponding alkylated or protonated salts;677 1C450a22. PFIB: 1,1,3,3,3-Pentafluoro-2-(trifluoromethyl)-1-propene (382-21-8);678 1C450a33. SEE MILITARY GOODS CONTROLS FOR BZ: 3-Quinuclidinyl benzilate (6581-06-2);679 1C450a44. Phosgene: Carbonyl dichloride (75-44-5);680 1C450a55. Cyanogen chloride (506-77-4);681 1C450a66. Hydrogen cyanide (74-90-8);682 1C450a77. Chloropicrin: Trichloronitromethane (76-06-2);684 1C3501C350 Chemicals, which may be used as precursors for toxic chemical agents, as follows, and "chemical mixtures" containing one or more thereof:685 1C350 44. SEE MILITARY GOODS CONTROLS FOR Methyl phosphonyl difluoride (676-99-3);1C350 2323. SEE MILITARY GOODS CONTROLS FOR Ethyl phosphonyl difluoride (753-98-0);686 1C350 2929. SEE MILITARY GOODS CONTROLS FOR O-Ethyl-2-diisopropylaminoethyl methyl phosphonite (QL) (57856-11-8);687 ML7c22. O-Alkyl (H or equal to or less than C10, including cycloalkyl) O-2-dialkyl (Methyl, Ethyl, n-Propyl or Isopropyl) aminoethyl alkyl (Methyl, Ethyl, n-Propyl or Isopropyl)phosphonites and corresponding alkylated and protonated salts, such as:QL: O-Ethyl-2-di-isopropylaminoethyl methylphosphonite (CAS 57856-11-8);688 ML7c33. Chlorosarin: O-Isopropyl methylphosphonochloridate (CAS 1445-76-7);689 ML7c44. Chlorosoman: O-Pinacolyl methylphosphonochloridate (CAS 7040-57-5);690 1C35 033. Dimethyl methylphosphonate (756-79-6);1C35 55. Methyl phosphonyl dichloride (676-97-1);1C350 1717.Diethyl ethylphosphonate (78-38-6);1C350 2121. Ethyl phosphinyl dichloride (1498-40-4);1C350 2222. Ethyl phosphonyl dichloride (1066-50-8);1C350 2626. Methyl phosphinyl dichloride (676-83-5);1C350 3333. Diethyl methylphosphonite (15715-41-0);1C350 3434. Dimethyl ethylphosphonate (6163-75-3);1C350 3535. Ethyl phosphinyl difluoride (430-78-4);1C350 3636. Methyl phosphinyl difluoride (753-59-3);1C350 5555. Methylphosphonic acid (993-13-5);1C350 5656. Diethyl methylphosphonate (683-08-9);1C350 6363. ethylphosphonothioic dichloride (676-98-2).691 1C350 5757. N,N-Dimethylaminophosphoryl dichloride (677-43-0);692 1C350 1818. Diethyl-N,N-dimethylphosphoramidate (2404-03-7);693 1C350 3131. Arsenic trichloride (7784-34-1);694 1C350 3232. Benzilic acid (76-93-7);695 1C350 1313. 3-Quinuclidinol (1619-34-7);696 1C350 1111. N,N-Diisopropyl-(beta)-aminoethyl chloride (96-79-7);1C350 5454. N,N-Diisopropyl-(Beta)-aminoethyl chloride hydrochloride (4261-68-1);697 1C350 2727. N,N-Diisopropyl-(beta)-amino ethanol (96-80-0);698 1C350 1212. N,N-Diisopropyl-(beta)-aminoethane thiol (5842-07-9);699 1C350 11. Thiodiglycol (111-48-8);700 1C350 2828. Pinacolyl alcohol (464-07-3);701 1C350 22. Phosphorus oxychloride (10025-87-3);702 1C350 77. Phosphorus trichloride (7719-12-2);703 1C350 3838. Phosphorus pentachloride (10026-13-8);704 1C350 88. Trimethyl phosphite (TMP) (121-45-9);705 1C350 3030. Triethyl phosphite (122-52-1);706 1C350 66. Dimethyl phosphite (DMP) (868-85-9);707 1C350 1919. Diethyl phosphite (762-04-9);708 1C350 5151. Sulphur monochloride (10025-67-9);709 1C350 5252. Sulphur dichloride (10545-99-0);710 1C350 99. Thionyl chloride (7719-09-7);711 1C350 5959. Ethyldiethanolamine (139-87-7);712 1C450b88. Methyldiethanolamine (105-59-9).713 1C350 4646. Triethanolamine (102-71-6);715 716 2B350aa. Reaction vessels or reactors, with or without agitators, with total internal (geometric) volume greater than 0.1 m3 (100 litres) and less than 20 m3 (20,000 litres), where all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:717 2B350a044. Nickel or alloys with more than 40% nickel by weight;718 2B350a011. Alloys with more than 25% nickel and 20% chromium by weight;719 2B350a022. Fluoropolymers;720 2B350a033. Glass (including vitrified or enamelled coating or glass lining);721 2B350a055. Tantalum or tantalum alloys;722 2B350a066. Titanium or titanium alloys;723 2B350a077. Zirconium or zirconium alloys; or724 2B350a088. Niobium (columbium) or niobium alloys;726 2B350cc. Storage tanks, containers or receivers with a total internal (geometric) volume greater than 0.1 m3 (100 litres) where all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:727 2B350c44. Nickel or alloys with more than 40% nickel by weight;728 2B350c11. Alloys with more than 25% nickel and 20% chromium by weight;729 2B350c22. Fluoropolymers;730 2B350c33. Glass (including vitrified or enamelled coatings or glass lining);731 2B350c55. Tantalum or tantalum alloys;732 2B350c66. Titanium or titanium alloys;733 2B350c77. Zirconium or zirconium alloys; or734 2B350c88. Niobium (columbium) or niobium alloys;736 2B350dd. Heat exchangers or condensers with a heat transfer surface area greater than 0.15 m2, and less than 20 m2; and tubes, plates, coils or blocks (cores) designed for such heat exchangers or condensers, where all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:737 2B350d55. Nickel or alloys with more than 40% nickel by weight;738 2B350d11. Alloys with more than 25% nickel and 20% chromium by weight;739 2B350d22. Fluoropolymers;740 2B350d33. Glass (including vitrified or enamelled coatings or glass lining);741 2B350d44. Graphite or 'carbon graphite';742 2B350d66. Tantalum or tantalum alloys;743 2B350d77. Titanium or titanium alloys;744 2B350d88. Zirconium or zirconium alloys;745 2B350d99. Silicon carbide;746 2B350d1010. Titanium carbide; or747 2B350d1111. Niobium (columbium) or niobium alloys;749

2B350dd. Heat exchangers or condensers with a heat transfer surface area greater than 0.15 m2, and less than 20 m2; and tubes, plates, coils or blocks (cores) designed for such heat exchangers or condensers, where all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials: 755 2B350ee. Distillation or absorption columns of internal diameter greater than 0.1 m; and liquid distributors, vapour distributors or liquid collectors designed for such distillation or absorbtion columns, where all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:756 2B350e55. Nickel or alloys with more than 40% nickel by weight;757 2B350e11. Alloys with more than 25% nickel and 20% chromium by weight;758 2B350e22. Fluoropolymers;759 2B350e33. Glass (including vitrified or enamelled coatings or glass lining);760 2B350e44. Graphite or 'carbon graphite';761 2B350e66. Tantalum or tantalum alloys;762 2B350e77. Titanium or titanium alloys;763 2B350e88. Zirconium or zirconium alloys; or764 2B350e99. Niobium (columbium) or niobium alloys;766

2B350ee. Distillation or absorption columns of internal diameter greater than 0.1 m; and liquid distributors, vapour distributors or liquid collectors designed for such distillation or absorbtion columns, where all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials: 770 2B350ff. Remotely operated filling equipment in which all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:771 2B350f022. Nickel or alloys with more than 40% nickel by weight;772 2B350f011. Alloys with more than 25% nickel and 20% chromium by weight; or773 2B350bb. Agitators for use in reaction vessels or reactors specified in 2B350.a.; and impellers, blades or shafts designed for such agitators, where all surfaces of the agitator that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:774 2B350b44. Nickel or alloys with more than 40% nickel by weight;775 2B350b11. Alloys with more than 25% nickel and 20% chromium by weight;776 2B350b22. Fluoropolymers;777 2B350b33. Glass (including vitrified or enamelled coatings or glass lining);778 2B350b55. Tantalum or tantalum alloys;779 2B350b66. Titanium or titanium alloys;780 2B350b77. Zirconium or zirconium alloys; or781 2B350b88. Niobium (columbium) or niobium alloys;782

2B350bb. Agitators for use in reaction vessels or reactors specified in 2B350.a.; and impellers, blades or shafts designed for such agitators, where all surfaces of the agitator that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials: 786 2B350gg. Valves with nominal sizes greater than 10 mm and casings (valve bodies) or preformed casing liners designed for such valves, in which all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:787 2B350g44. Nickel or alloys with more than 40% nickel by weight;788 2B350g11. Alloys with more than 25% nickel and 20% chromium by weight;789 2B350g22. Fluoropolymers;790 2B350g33. Glass (including vitrified or enamelled coatings or glass lining);791 2B350g55. Tantalum or tantalum alloys;792 2B350g66. Titanium or titanium alloys;793 2B350g77. Zirconium or zirconium alloys; or794 2B350g88. Niobium (columbium) or niobium alloys;795 2B350g99. Ceramic materials as follows:796 2B350g9aa. Silicon carbide with purity of 80 % or more by weight;797 2B350g9bb. Aluminium oxide (alumina) with purity of 99,9 % or more by weight;798 2B350g9cc. Zirconium oxide (zirconia);800

2B350gg. Valves with nominal sizes greater than 10 mm and casings (valve bodies) or preformed casing liners designed for such valves, in which all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials: 803 2B350hh. Multi-walled piping incorporating a leak detection port, in which all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:804 2B350h055. Nickel or alloys with more than 40% nickel by weight;805 2B350h11. Alloys with more than 25% nickel and 20% chromium by weight;806 2B350h22. Fluoropolymers;807 2B350h33. Glass (including vitrified or enamelled coatings or glass lining);808 2B350h44. Graphite or 'carbon graphite';809 2B350h66. Tantalum or tantalum alloys;810 2B350h77. Titanium or titanium alloys;811 2B350h88. Zirconium or zirconium alloys; or812 2B350h99. Niobium (columbium) or niobium alloys;813 2B350ii. Multiple-seal and seal-less pumps, with manufacturer's specified maximum flow-rate greater than 0.6 m3/hour, or vacuum pumps with manufacturer's specified maximum flow-rate greater than 5 m3/hour (under standard temperature (273 K (0 C)) and pressure (101.3 kPa) conditions); and casings (pump bodies), preformed casing liners, impellers, rotors or jet pump nozzles designed for such pumps, in which all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:814 2B350i77. Nickel or alloys with more than 40% nickel by weight;815 2B350i11. Alloys with more than 25% nickel and 20% chromium by weight;816 2B350i44. Fluoropolymers;817 2B350i55. Glass (including vitrified or enamelled coatings or glass lining);818 2B350i66. Graphite or 'carbon graphite';819 2B350i88. Tantalum or tantalum alloys;820 2B350i99. Titanium or titanium alloys;821 2B350i1010. Zirconium or zirconium alloys; or822 2B350i22. Ceramics;823 2B350i33. Ferrosilicon;824 2B350i1111. Niobium (columbium) or niobium alloys;826

2B350ii. Multiple-seal and seal-less pumps, with manufacturer's specified maximum flow-rate greater than 0.6 m3/hour, or vacuum pumps with manufacturer's specified maximum flow-rate greater than 5 m3/hour (under standard temperature (273 K (0 C)) and pressure (101.3 kPa) conditions); and casings (pump bodies), preformed casing liners, impellers, rotors or jet pump nozzles designed for such pumps, in which all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials: 832 2B350jj. Incinerators designed to destroy chemicals specified in entry 1C350, having specially designed waste supply systems, special handling facilities and an average combustion chamber temperature greater than 1,273 K (1,000), in which all surfaces in the waste supply system that come into direct contact with the waste products are made from or lined with any of the following materials:833 2B350j33. Nickel or alloys with more than 40% nickel by weight.834 2B350j11. Alloys with more than 25% nickel and 20% chromium by weight;835 2B350j22. Ceramics;837 2B3512B351 Toxic gas monitoring systems, other than those specified in 1A004, as follows; and dedicated detectors therefor:838 2B351aa. Designed for continuous operation and usable for the detection of chemical warfare agents or chemicals specified in 1C350, at concentrations of less than 0.3 mg/m3; or839 2B351bb. Designed for the detection of cholinesterase-inhibiting activity.841

EU 212846848 1C3511C3521C3541C351 Human pathogens, zoonoses and toxins, as follows: Note: 1C351 does not control vaccines or immunotoxins.

1C352 Animal pathogens, as follows: Note: 1C352 does not control vaccines.

1C354 Plant pathogens, as follows:1C352a1717. African horse sickness virus.1C352a11. African swine fever virus;1C351a55. Ebola virus;1C351a1919. Yellow fever virus;1C352a66. Porcine herpes virus (Aujeszky's disease);1C351a2424. Omsk haemorrhagic fever virus;1C351a2525. Oropouche virus;1C351a2121. Kyasanur Forest virus;1C352a1212. Rinderpest virus;1C352a88. Lyssa virus;1C351a22. Congo-Crimean haemorrhagic fever virus;1C352a44. Foot and mouth disease virus;1C351a1212. Monkey pox virus;1C352a1010. Peste des petits ruminants virus;1C352a1515. Vesicular stomatitis virus;1C351a1717. Western equine encephalitis virus;1C351a2828. St Louis encephalitis virus;1C351a1414. Tick-borne encephalitis virus (Russian Spring-Summer encephalitis virus);1C351a11. Chikungunya virus;1C351a2222. Louping ill virus;1C352a1414. Teschen disease virus;1C351a33. Dengue fever virus;1C351a1515. Variola virus;1C351a44. Eastern equine encephalitis virus;1C352a22. Avian influenza virus, which are:1C352a77. Swine fever virus (Hog cholera virus);1C351a3232. Nipah virus;1C351a2020. Japanese encephalitis virus;1C352a99. Newcastle disease virus;1C351a3131. Pulmonary & renal syndrome-haemorrhagic fever viruses (Seoul, Dobrava, Puumala, Sin Nombre);1C351a66. Hantaan virus;1C352a1111. Porcine enterovirus type 9 (swine vesicular disease virus);1C351a77. Junin virus;1C352a033. Bluetongue virus;1C351a1616. Venezuelan equine encephalitis virus;1C351a2929. Hendra virus (Equine morbillivirus);1C354a11. Potato Andean latent tymovirus;1C354a22. Potato spindle tuber viroid;1C351a2626. Powassan virus;1C351a1010. Machupo virus;1C351a1111. Marburg virus;1C351a2323. Murray Valley encephalitis virus;1C351a3030. South American haemorrhagic fever (Sabia, Flexal, Guanarito);1C352a55. Goat pox virus;1C352a1313. Sheep pox virus;1C351a138. Lassa fever virus;1C352a1616. Lumpy skin disease virus;1C351a813. Rift Valley fever virus;1C351a99. Lymphocytic choriomeningitis virus;1C351a27850 1C3511C3521C351 Human pathogens, zoonoses and toxins, as follows: Note: 1C351 does not control vaccines or immunotoxins.

1C352 Animal pathogens, as follows: Note: 1C352 does not control vaccines1C351c22. Brucella abortus;1C351c55. Chlamydia psittaci;1C351c1414. Clostridium perfringens epsilon toxin producing types;1C351b11. Coxiella burnetii;1C352b11. Mycoplasma mycoides subspecies mycoides SC (small colony);1C351c1212. Vibrio cholerae;1C351b22. Bartonella quintana (Rochalimaea quintana, Rickettsia quintana);1C351c1111. Shigella dysenteriae;1C351c11. Bacillus anthracis; 1C351c1010. Salmonella typhi;1C351c1515. Enterohaemorrhagic Escherichia coli, serotype O157 and other verotoxin producing serotypes;1C351b33. Rickettsia prowasecki;1C351c88. Burkholderia mallei (Pseudomonas mallei);1C351c44. Brucella suis;1C351c1313. Yersinia pestis;1C351c66. Clostridium botulinum;1C351c33. Brucella melitensis;F1C352b22. Mycoplasma capricolum subspecies capripneumoniae.1C351c77. Francisella tularensis;1C351c99. Burkholderia pseudomallei (Pseudomonas pseudomallei);1C351b44. Rickettsia rickettsii;852 1C3511C351d1C351 Human pathogens, zoonoses and toxins, as follows: d. Toxins, as follows, and sub-unit of toxins thereof: Note: 1C351 does not control vaccines or immunotoxins.1C351d1111. Aflatoxins;1C351d1212. Abrin;1C351d022. Clostridium perfringens toxins;-1C351d1616. HT-2 toxin;1C351d77. Staphylococcus aureus toxins;1C351d33. Conotoxin;1C351d1313. Cholera toxin;1C351d66. Shiga toxin;1C351d1414. Diacetoxyscirpenol toxin;-1C351d1515. T-2 toxin;1C351d88. Tetrodotoxin;1C351d1919. Viscum album Lectin 1 (Viscumin);1C351d99. Verotoxin and shiga-like ribosome inactivating proteins;1C351d11. Botulinum toxins;1C351d1818. Volkensin;1C351d1010. Microcystin (Cyanginosin);1C351d1717. Modeccin;854 1C351dd. Toxins, as follows, and sub-unit of toxins thereof:855 1C3511C3541C351 Human pathogens, zoonoses and toxins, as follows:

1C354 Plant pathogens, as follows:1C354b44. Clavibacter michiganensis subsp. Sepedonicus (Corynebacterium michiganensis subsp. Sepedonicum or Corynebacterium Sepedonicum);1C351e11. Coccidioides immitis;1C351e22. Coccidioides posadasii.1C354c22. Cochliobolus miyabeanus (Helminthosporium oryzae);1C354c11. Colletotrichum coffeanum var. virulans (Colletotrichum kahawae);1C354b11.Xanthomonas albilineans;1C354b33. Xanthomonas oryzae pv. Oryzae (Pseudomonas campestris pv. Oryzae);1C354b22. Xanthomonas campestris pv. citri including strains referred to as Xanthomonas campestris pv. citri types A,B,C,D,E or otherwise classified as Xanthomonas citri, Xanthomonas campestris pv. aurantifolia or Xanthomonas campestris pv. citrumelo;1C354c66. Magnaporthe grisea (pyricularia grisea/pyricularia oryzae).1C354c44. Puccinia graminis (syn. Puccinia graminis f. sp. tritici);1C354c55. Puccinia striiformis (syn. Puccinia glumarum);1C354c33. Microcyclus ulei (syn. Dothidella ulei);1C354b55 Ralstonia solanacearum Races 2 and 3 (Pseudomonas solanacearum Races 2 and 3 or Burkholderia solanacearum Races 2 and 3);857 1C353aa. Genetically modified organisms or genetic elements that contain nucleic acid sequences associated with pathogenicity of organisms specified in 1C351.a., 1C351.b., 1C351.c, 1C351.e., 1C352 or 1C354;1C353bb. Genetically modified organisms or genetic elements that contain nucleic acid sequences coding for any of the "toxins" specified in 1C351.d. or "sub-units of toxins" thereof.1C353Y11. Genetic elements include, inter alia, chromosomes, genomes, plasmids, transposons and vectors whether genetically modified or unmodified.858 1C353aa. Genetically modified organisms or genetic elements that contain nucleic acid sequences associated with pathogenicity of organisms specified in 1C351.a., 1C351.b., 1C351.c, 1C351.e., 1C352 or 1C354;1C353bb. Genetically modified organisms or genetic elements that contain nucleic acid sequences coding for any of the "toxins" specified in 1C351.d. or "sub-units of toxins" thereof.860 861 2B352aa. Complete biological containment facilities at P3, P4 containment level;2B352f22. Class III biological safety cabinets or isolators with similar performance standards;862 2B352aa. Complete biological containment facilities at P3, P4 containment level;863 2B352f22. Class III biological safety cabinets or isolators with similar performance standards;865 2B352bb. Fermenters capable of cultivation of pathogenic "microorganisms", viruses or capable of toxin production, without the propagation of aerosols, and having a total capacity of 20 litres or more;866 2B352cc. Centrifugal separators, capable of continuous separation without the propagation of aerosols, having all the following characteristics:867 2B352c11 Flow rate exceeding 100 litres per hour;868 2B352c22 Components of polished stainless steel or titanium;869 2B352c33 One or more sealing joints within the steam containment area; and870 2B352c44 Capable of in-situ steam sterilisation in a closed state;872 ()2B352dd. Cross (tangential) flow filtration equipment and components as follows:2B352dXNote: 2B352.d. does not control reverse osmosis equipment, as specified by the manufacturer.873 2B352d1aa. A total filtration area equal to or greater than 1 m2; and874 ()()2B352d1bb. Having any of the following characteristics8752B352d1b11. Capable of being sterilised or disinfected in-situ; or876()2B352d01b22. Using disposable or single-use filtration components;878 2B352d22. Cross (tangential) flow filtration components (e.g. modules, elements, cassettes, cartridges, units or plates) with filtration area equal to or greater than 0.2 m2 for each component and designed for use in cross (tangential) flow filtration equipment specified in 2B352.d.;879 2B352ee. Steam sterilisable freeze drying equipment with a condenser capacity exceeding 10 kg of ice in 24 hours and less than 1,000 kg of ice in 24 hours;880 ''881 883 2B352f011. Protective full or half suits, or hoods dependent upon a tethered external air supply and operating under positive pressure;884 2B352gg. Chambers designed for aerosol challenge testing with "microorganisms", viruses or "toxins" and having a capacity of 1 m3 or greater.885 9A3509A350 Spraying or fogging systems, specially designed or modified for fitting to aircraft, "lighter-than-air vehicles" or unmanned aerial vehicles, and specially designed components therefor, as follows:886 '9A350aa. Complete spraying or fogging systems capable of delivering, from a liquid suspension, an initial droplet 'VMD' of less than 50m at a flow rate of greater than two litres per minute;9A350cXNote: Aerosol generating units are devices specially designed or modified for fitting to aircraft such as nozzles, rotary drum atomizers and similar devices.887 9A350bb. Spray booms or arrays of aerosol generating units capable of delivering, from a liquid suspension, an initial droplet 'VMD' of less than 50m at a flow rate of greater than two litres per minute;9A350cXNote: Aerosol generating units are devices specially designed or modified for fitting to aircraft such as nozzles, rotary drum atomizers and similar devices.888 9A350cc. Aerosol generating units specially designed for fitting to systems specified in 9A350.a. and b.890 891 9A1049A104 Sounding rockets, capable of a range of at least 300 km.9B1169B116 Specially designed production facilities for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111,or 9A116 to 9A120.892 9A012Unmanned aerial vehicles (UAVs), associated systems, equipment and components, as follows:a. UAVs having any of the following: b. Associated systems, equipment and components, as follows893 894 895 897 7B0037B003 Equipment specially designed for the "production" of equipment specified in 7A.EU

9B1159B115 Specially designed production equipment for the systems, sub-systems and components specified in 9A005to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.9B1169B116 Specially designed "production facilities" for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, or 9A116 to 9A120.898 899 9A1199A119 Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109.900 9A105bb. Liquid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005 or 9A105.a., having a total impulse capacity equal to or greater than 0.841 MNs.9A105aa. Liquid propellant rocket engines usable in missiles, other than those specified in 9A005, having a total impulse capacity equal to or greater than 1,1 MNs;9A1079A107 Solid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A007, having total impulse capacity equal to or greater than 0.841 MNs.901 902 9A116aa. Reentry vehicles;903 9A116bb. Heat shields and components therefor fabricated of ceramic or ablative materials;904 9A116cc. Heat sinks and components therefor fabricated of light-weight, high heat capacity materials;905 9A116dd. Electronic equipment specially designed for reentry vehicles.906 7A1177A117 "Guidance sets", usable in "missiles" capable of achieving system accuracy of 3.33% or less of the range (e.g., a "CEP" of 10 km or less at a range of 300 km).907 9A106c9A106 Systems or components, other than those specified in 9A006 as follows, specially designed for liquid rocketpropulsion systems:c. Thrust vector control sub-systems, usable in missiles;9A108c9A108 Components, other than those specified in 9A008, as follows, specially designed for solid rocket propulsion systems c. Thrust vector control sub-systems, usable in missiles.908 9B1159B115 Specially designed production equipment for the systems, sub-systems and components specified in 9A005to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.EU

909 9A1019A101 Turbojet and turbofan engines (including turbocompound engines), other than those specified in 9A001, as follows;910 9A101a11. Maximum thrust value greater than 400 N (achieved un-installed) excluding civil certified engines with a maximum thrust value greater than 8,890 N (achieved un-installed), and911 9A101a22. Specific fuel consumption of 0.15 kg/N/hr or less (at maximum continuous power at sea level static and standard conditions);912 9A1119A111 Pulse jet engines, usable in "missiles" or unmanned aerial vehicles specified in 9A012, and specially designed components therefor.9A0119A011Ramjet, scramjet or combined cycle engines, and specially designed components therefor.913 9A108aa. Rocket motor cases and insulation components therefor, usable in missiles, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;914 9C1089C108 "Insulation" material in bulk form and "interior lining", other than those specified in 9A008, for rocket motor cases usable in "missiles" or specially designed for 'missiles'.915 9A108aa. Rocket motor cases and insulation components therefor, usable in missiles, space launch vehiclesspecified in 9A004 or sounding rockets specified in 9A104;9C1089C108 "Insulation" material in bulk form and "interior lining", other than those specified in 9A008, for rocket motor cases usable in "missiles" or specially designed for 'missiles'.916 9A108bb. Rocket nozzles, usable in missiles, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;917 9A106dd. Liquid and slurry propellant (including oxidisers) control systems, and specially designed components therefor, designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz.918 ( 29A1099A109 Hybrid rocket motors, usable in 'missiles', other than those specified in 9A009, and specially designed components therefor.919 9A1209A120 Liquid propellant tanks, other than those specified in 9A006, specially designed for propellants specified in 1C111 or 'other liquid propellants', used in rocket systems capable of delivering at least a 500 kg payload to a range of at least 300 km.920921922 9A1029A102 Turboprop engine systems specially designed for unmanned aerial vehicles specified in 9A012, and speciallydesigned components therefor, having a maximum power greater than 10 kW.9A102XNote: 9A102 does not control civil certified engines.924 9A1179A117 Staging mechanisms, separation mechanisms, and interstages, usable in "missiles".9B1159B115 Specially designed production equipment for the systems, sub-systems and components specified in 9A005to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.925 2B1092B109 Flow-forming machines, other than those specified in 2B009, and specially designed components as follows:2B109a11. According to the manufacturer's technical specification, can be equipped with numerical control units or a computer control, even when not equipped with such units; and2B109a22. With more than two axes which can be coordinated simultaneously for contouring control.2B109bb. Specially designed components for flow-forming machines specified in 2B009 or 2B109.a.926 927 9A106dXNote: The only servo valves and pumps specified in 9A106.d., are the following:928 9A106dd. Liquid and slurry propellant (including oxidisers) control systems, and specially designed components therefor, designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz.929 9A106dXaa. Servo valves designed for flow rates equal to or greater than 24 litres per minute, at an absolute pressure equal to or greater than 7 MPa, that have an actuator response time of less than 100 ms;930 9A106dXbb. Pumps, for liquid propellants, with shaft speeds equal to or greater than 8,000 r.p.m. or with discharge pressures equal to or greater than 7 MPa.931

2A001b2A001 Anti-friction bearings and bearing systems, as follows, and components therefor:b. Other ball bearings and solid roller bearings, having all tolerances specified by the manufacturer in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or RBEC-9, or other national equivalents), or better;932 933 934 936 1C1111C111 Propellants and constituent chemicals for propellants, other than those specified in 1C011, as follows:ML8ML8 Energetic materials, and related substances, as follows:937 ML8C4aa. Hydrazine (CAS 302-01-2) in concentrations of 70 % or more;938 1C111a44. Hydrazine derivatives as follows:ML8c44. Hydrazine and derivatives, as follows (see also ML8d8 and d9 for oxidising hydrazine derivatives):ML8c4a939 ML8d22. AP (ammonium perchlorate) (CAS 7790-98-9);940 ML8d11. ADN (ammonium dinitramide or SR 12) (CAS 140456-78-6);941 1C111a11. Spherical aluminium powder, other than that specified in the Military Goods Controls, with particles of uniform diameter of less than 200m and an aluminium content of 97% by weight or more, if at least 10% of the total weight is made up of particles of less than 63m, according to ISO 2591:1988 or national equivalents;EUML8c8 942 1C111a22. Metal fuels, other than that specified in the Military Goods Controls, in particle sizes of less than 60 um, whether spherical, atomized, spheroidal, flaked or ground, consisting 97% by weight or more of any of the following:EUML8c51C111a2aa. Zirconium;1C111a2bb. Beryllium;1C111a2cc. Magnesium; or1C111a2dd. Alloys of the metals specified in a. to c. above;943 1C011b1C011 Metals and compounds, as follows:

b. Boron or boron carbide of 85 % purity or higher, and a particle size of 60 m or less;ML8c5b22. Boron (CAS 7440-42-8) or boron carbide (CAS 12069-32-8) fuels of 85 % purity or higher and particle sizes of less than 60 m;944 ML8c77. Perchlorates, chlorates and chromates, composited with powdered metal or other high energyfuel components;945 1C111c11. SEE MILITARY GOODS CONTROLS FOR Carboranes, decaboranes, pentaboranes and derivatives thereof;ML8c3c. Pyrotechnics, fuels and related substances, as follows, and mixtures thereof: 3. Carboranes; decaborane (CAS 17702-41-9); pentaboranes (CAS 19624-22-7 and 18433-84-6) and their derivatives;946 1C111a33. Oxidiser substances usable in liquid propellant rocket engines as follows:947 1C111a3aa. Dinitrogen trioxide(CAS 10544-73-7);948 1C111a3bb. Nitrogen dioxide(CAS 10102-44-0)/dinitrogen tetroxide (CAS 10544-72-6);949 1C111a3cc. Dinitrogen pentoxide(CAS 10102-03-1);950) 1C111a3dd. Mixed Oxides of Nitrogen (MON);951) 1C111a3ee. SEE MILITARY GOODS CONTROLS FOR Inhibited Red Fuming Nitric Acid (IRFNA);ML8d1010. Liquid oxidisers comprised of or containing inhibited red fuming nitric acid (IRFNA) (CAS8007-58-7);952 1C111a3ff. SEE MILITARY GOODS CONTROLS AND 1C238 FOR Compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen;ML8d33. Compounds composed of fluorine and any of the following:a. Other halogens;b. Oxygen; orc. Nitrogen; Note 2: ML8.d.3 does not apply to nitrogen trifluoride in its gaseous state.953 1C111011. Carboxy-terminated polybutadiene (CTPB);954 1C111b22. Hydroxy-terminated polybutadiene (HTPB), other than that specified in the Military Goods Controls;EUML8c12955 ML8e1111. GAP (glycidylazide polymer) (CAS 143178-24-9) and its derivatives;956 1C111b33 Polybutadiene-acrylic acid (PBAA);957 1C111b44 Polybutadiene-acrylic acid-acrylonitrile (PBAN);958 959 960 961 ML8f1111. MAPO (tris-1-(2-methyl)aziridinyl phosphine oxide) (CAS 57-39-6); BOBBA 8 (bis (2-methylaziridinyl) 2-(2-hydroxypropanoxy) propylamino phosphine oxide); and other MAPO derivatives;962 ML8f2121. TEPANOL (tetraethylenepentaamineacrylonitrileglycidol) (CAS 68412-46-4); cyanoethylated polyamines adducted with glycidol and their salts;963 ML8f2020. TEPAN (tetraethylenepentaamineacrylonitrile) (CAS 68412-45-3); cyanoethylated polyaminesand their salts;964 ML8f1717. Polyfunctional aziridine amides with isophthalic, trimesic (BITA or butylene imine trimesamide), isocyanuric or trimethyladipic backbone structures and 2-methyl or 2-ethyl substitutions on the aziridine ring;965 ML8f2222. TPB (triphenyl bismuth) (CAS 603-33-8).966 1C111c66. Ferrocene derivatives as follows:967 1C111c22. Triethylene glycol dinitrate (TEGDN)(CAS 111-22-8);968 1C111c44. Trimethylolethane trinitrate (TMETN) (CAS 3032-55-1);969 ML8e55. BTTN (butanetrioltrinitrate) (CAS 6659-60-5) (see also ML8.g.8. for its precursors);970 1C111c55. Diethylene glycol dinitrate (DEGDN)(CAS 693-21-0);971 1C111b55 Polytetrahydrofuran polyethylene glycol (TPEG);9721C111c77. 4,5 diazidomethyl-2-methyl-1,2,3-triazole (iso- DAMTR), other than that specified in the Military Goods Controls.973ML8e1414. NENAs (nitratoethylnitramine compounds) (CAS 17096-47-8, 85068-73-1, 82486-83-7,82486-82-6 and 85954-06-9);974975976ML8e33. BDNPA (bis (2,2-dinitropropyl)acetal) (CAS 5108-69-0);977ML8e44. BDNPF (bis (2,2-dinitropropyl)formal) (CAS 5917-61-3);979 1B1151B115 Equipment, other than that specified in 1B002 or 1B102, for the production of propellant and propellant constituents, as follows, and specially designed components therefor: a. "Production equipment" for the "production", handling or acceptance testing of liquid propellants or propellant constituents specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls; b. "Production equipment" for the "production", handling, mixing, curing, casting, pressing, machining, extruding or acceptance testing of solid propellants or propellant constituents specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls.

81B1021B102 Metal powder production equipment, other than that specified in 1B002, and components as follows:a. Metal powder production equipment usable for the production, in a controlled environment, ofspherical or atomised materials specified in 1C011.a., 1C011.b., 1C111.a.1., 1C111.a.2. or in the Military Goods Controls.b. Specially designed components for production equipment specified in 1B002 or 1B102.a.980 981 ML8a13a13. HMX and derivatives (see also ML8.g.5. for its precursors), as follows: a. HMX (Cyclotetramethylenetetranitramine, octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazine,1,3,5,7-tetranitro-1,3,5,7-tetraza-cyclooctane, octogen or octogene) (CAS 2691-41-0);ML8a21a21. RDX and derivatives, as follows: a. RDX (cyclotrimethylenetrinitramine, cyclonite, T4, hexahydro-1,3,5-trinitro-1,3,5-triazine, 1,3,5-trinitro-1,3,5-triaza-cyclohexane, hexogen or hexogene) (CAS 121-82-4);982 983 1C111c33. 2-Nitrodiphenylamine (CAS 119-75-5);ML8f1313. N-methyl-p-nitroaniline (CAS 100-15-2);984 ML8d77. HNF (hydrazinium nitroformate) (CAS 20773-28-8);985 ML8a44. CL-20 (HNIW or Hexanitrohexaazaisowurtzitane) (CAS 135285-90-4); chlathrates of CL-20(see also ML8.g.3. and g.4. for its precursors);987 ()1B1171B117 Batch mixers with provision for mixing under vacuum in the range of zero to 13.326 kPa and with temperature control capability of the mixing chamber and having all of the following, and specially designed components therefor:988 1B117aa. A total volumetric capacity of 110 litres or more; and989 1B117bb. At least one mixing/kneading shaft mounted off centre.991 ()1B1181B118 Continuous mixers with provision for mixing under vacuum in the range of zero to 13.326 kPa and with a temperature control capability of the mixing chamber having any of the following, and specially designed components therefor:992 1B118aa. Two or more mixing/kneading shafts; or993 1B118bb. A single rotating shaft which oscillates and having kneading teeth/pins on the shaft as well as inside the casing of the mixing chamber.995 1B1191B119 Fluid energy mills usable for grinding or milling substances specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls, and specially designed components therefor.996 1B1021B102 Metal powder "production equipment", other than that specified in 1B002, and components as follows: a. Metal powder "production equipment" usable for the "production", in a controlled environment, of spherical or atomised materials specified in 1C011.a., 1C011.b., 1C111.a.1., 1C111.a.2. or in the Military Goods Controls. b. Specially designed components for "production equipment" specified in 1B002 or 1B102.a.997 1B1011B101 Equipment, other than that specified in 1B001, for the "production" of structural composites as follows; and specially designed components and accessories therefor:998 1B101aa. Filament winding machines of which the motions for positioning, wrapping and winding fibres can be coordinated and programmed in three or more axes, designed to fabricate composite structures or laminates from fibrous or filamentary materials, and coordinating and programming controls;999 1B101bb. Tape-laying machines of which the motions for positioning and laying tape and sheets can be coordinated and programmed in two or more axes, designed for the manufacture of composite airframe and "missile" structures;1000 1B001cc. Multidirectional, multidimensional weaving machines or interlacing machines, including adapters andmodification kits, for weaving, interlacing or braiding fibres, to manufacture composite structures;1001 1B101cc. Equipment designed or modified for the "production" of "fibrous or filamentary materials" as follows:1002 1B101c11. Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon or polycarbosilane) including special provision to strain the fibre during heating;1003 1B101c22. Equipment for the vapour deposition of elements or compounds on heated filament substrates;1004 1B101c33. Equipment for the wet-spinning of refractory ceramics (such as aluminium oxide);1005 1B101dd. Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms specified in entry 9C110.1007 1B1161B116 Specially designed nozzles for producing pyrolitically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1,573 K (1,300 C) to 3,173 K (2,900 C) temperature range at pressures of 130 Pa to 20 kPa.1008 2B1172B117 Equipment and process controls, other than those specified in 2B004, 2B005.a., 2B104 or 2B105, designed or modified for densification and pyrolysis of structural composite rocket nozzles and reentry vehicle nose tips.1009 1010 1011 2B1042B104 "Isostatic presses", other than those specified in 2B004, having all of the following:1012 2B104aa. Maximum working pressure of 69 MPa or greater;1013 2B104bb. Designed to achieve and maintain a controlled thermal environment of 873 K (600C) or greater; and1014 2B104cc. Possessing a chamber cavity with an inside diameter of 254 mm or greater.1015 2B1052B105 Chemical vapour deposition (CVD) furnaces, other than those specified in 2B005.a., designed or modified for the densification of carbon-carbon composites.1016 1017 9A1109A110 Composite structures, laminates and manufactures thereof, other than those specified in 9A010, speciallydesigned for use in missiles or the subsystems specified in 9A005, 9A007, 9A105, 9A106.c., 9A107,9A108.c., 9A116 or 9A119.9C1109C110 Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for composite structures, laminates and manufactures specified in 9A110, made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a "specific tensile strength" greater than 7.62 x 10(4) m and a "specific modulus" greater than 3.18 x 10(6) m.9C110XNote: The only resin impregnated fibre prepregs specified in entry 9C110 are those using resins with a glass transition temperature (Tg ), after cure, exceeding 418 K (145 C) as determined by ASTM D4065 or equivalent.1018 1A1021A102 Resaturated pyrolized carbon-carbon components designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.1C1021C102 Resaturated pyrolized carbon-carbon materials designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.1019 1C1071C107 Graphite and ceramic materials, other than those specified in 1C007, as follows:1020 1C107aa. Fine grain graphites with a bulk density of 1.72 g/cm3 or greater, measured at 288 K (15 C), and having a grain size of 100 um or less, usable for rocket nozzles and re-entry vehicle nose tips, which can be machined to any of the following products:1021 1C107a11. Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater;1C107a22. Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; or10222 1C107a33. Blocks having a size of 120 mm x 120 mm x 50 mm or greater;1023 1C107bb. Pyrolytic or fibrous reinforced graphites, usable for rocket nozzles and reentry vehicle nose tips usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;1024 1025 1C107cc. Ceramic composite