Council Regulation (EC) No 329/2007 of 27 March 2007 concerning restrictive measures against the Democratic People's Republic of Korea (repealed)
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Version Superseded: 31/07/2009
Point in time view as at 10/02/2008.
There are currently no known outstanding effects by UK legislation for Council Regulation (EC) No 329/2007 (repealed),
ANNEX I
.
Textual Amendments
Where possible, the items in this Annex are defined by reference to the list of dual-use items set out in Annex I to Council Regulation (EC) No 1334/2000, as amended by Council Regulation (EC) No 1183/2007 (1) .
The descriptions of the items in this Annex are often, but not always, identical or similar to descriptions of the items set out in the list of dual-use items. Each description is based as much as possible on that of the first dual-use item referred to. Where there are differences between the two descriptions, the description of the goods or technology found in this Annex shall be decisive. For the sake of clarity, an asterisk indicates that a description is based on the description of the dual-use item referred to, but contains different values for the technical parameters used or omits or adds specific elements.
If only part of the scope of the dual-use item referred to is covered by an entry in this Annex, the reference number taken from the list of dual-use items is preceded by ‘ ex ’.
For the definitions of terms between ‘ double quotation marks ’ please refer to Regulation (EC) No 1183/2007.
This Annex does not include goods and technology (including software) included in the Common Military List of the European Union (2) . In accordance with Article 1(1)(a) of Common Position 2006/795/CFSP (3) , the Member States of the European Union will prohibit the direct or indirect supply, sale or transfer of such goods and technology to the Democratic People’s Republic of Korea.
N.B.: In judging whether the prohibited component or components are to be considered the principal element, it is necessary to weigh the factors of quantity, value and technological know-how involved and other special circumstances which might establish the prohibited component or components as the principal element of the goods being procured. U.K.
(To be read in conjunction with Section I.0.B.)
The sale, supply, transfer or export of ‘ technology ’ directly associated with any goods whose sale, supply, transfer or export is prohibited in Section I.0.A is prohibited according to the provisions of Category I.0.
‘ Technology ’ for the ‘ development ’ , ‘ production ’ or ‘ use ’ of goods under prohibition remains under prohibition even when applicable to non-prohibited goods.
The approval of goods for export granted in accordance with Article 5 of Regulation (EC) No 329/2007, also authorizes the export to the same end-user of the minimum ‘ technology ’ required for the installation, operation, maintenance and repair of the goods.
Prohibitions on ‘ technology ’ transfer do not apply to information ‘ in the public domain ’ or to ‘ basic scientific research ’ .
(To be read in conjunction with Sections I.1B, I.2B, I.3B, I.4B, I.5B, I.6B, I.7B and I.9B.)
The sale, supply, transfer or export of ‘ technology ’ which is ‘ required ’ for the ‘ development ’ , ‘ production ’ or ‘ use ’ of goods whose sale, supply, transfer or export is prohibited in Categories I.1 to I.9, is prohibited according to the provisions of Categories I.1 to I.9.
‘ Technology ’ ‘ required ’ for the ‘ development ’ , ‘ production ’ or ‘ use ’ of goods under prohibition remains under prohibition even when applicable to non-prohibited goods.
Prohibitions do not apply to that ‘ technology ’ which is the minimum necessary for the installation, operation, maintenance (checking) and repair of those goods which are not prohibited or whose export has been authorised in accordance with Regulation (EC) No 329/2007.
Prohibitions on ‘ technology ’ transfer do not apply to information ‘ in the public domain ’ , to ‘ basic scientific research ’ or to the minimum necessary information for patent applications.
(This note overrides any prohibition within sections I.0B, I.1B, I.2B, I.3B, I.4B, I.5B, I.6B, I.7B and I.9B.)
Categories I.0 to I.9 of this list do not prohibit ‘ software ’ which is either:
Generally available to the public by being:
Sold from stock at retail selling points, without restriction, by means of:
Over-the-counter transactions;
Mail order transactions;
Electronic transactions; or
Telephone order transactions; and
Designed for installation by the user without further substantial support by the supplier; or
‘ In the public domain ’ .
| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|---|---|
| I.0B.001 | 0D001 | ‘ Software ’ specially designed or modified for the ‘ development ’ , ‘ production ’ or ‘ use ’ of goods specified in Section I.0A. |
| I.0B.002 | 0E001 | ‘ Technology ’ according to the Nuclear Technology Note for the ‘ development ’ , ‘ production ’ or ‘ use ’ of goods specified in Section I.0A. |
| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|---|---|
| I.1A.001 | 1A102 | Resaturated pyrolized carbon-carbon components designed for space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005. N.B.: See also Military Goods Controls for components for rockets and missiles. |
| I.1A.002 | 1A202 | Composite structures in the form of tubes and having both of the following characteristics: N.B.: See also I.9A.011. a. An inside diameter of between 75 mm and 400 mm; and b. Made with any of the ‘ fibrous or filamentary materials ’ specified in I.1A.024 or I.1A.034.a. or with carbon prepreg materials specified in I.1A.034.c. |
| I.1A.003 | 1A225 | 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. |
| I.1A.004 | 1A226 | 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; and b. Designed to be used in vacuum distillation towers. |
| I.1A.005 | 1A227 | High-density (lead glass or other) radiation shielding windows, having all of the following characteristics, and specially designed frames therefor: a. A ‘cold area’ greater than 0,09 m 2 ; b. A density greater than 3 g/cm 3 ; and c. A thickness of 100 mm or greater. Technical Note:In I.1A.005 the term ‘ cold area ’ means the viewing area of the window exposed to the lowest level of radiation in the design application. |
| I.1A.006 | ex 1B001* (1B001.a, ex 1B001.b and 1B001.c) | Equipment for the production of fibres, prepregs, preforms or ‘ composites ’ specified in I.1A.024, as follows, and specially designed components and accessories therefor: N.B.: See also I.1A.007 and I.1A.014.
|
| I.1A.007 | 1B101 and ex 1B001.d | Equipment, other than that specified in I.1A.006, for the ‘ production ’ of structural composites as follows; and specially designed components and accessories therefor: Note: Components and accessories specified in I.1A.007 include moulds, mandrels, dies, fixtures and tooling for the preform pressing, curing, casting, sintering or bonding of composite structures, laminates and manufactures thereof. a. 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; b. 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; c. Equipment designed or modified for the ‘ production ’ of ‘ fibrous or filamentary materials ’ as follows: 1. Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon or polycarbosilane) including special provision to strain the fibre during heating; 2. Equipment for the vapour deposition of elements or compounds on heated filament substrates; 3. Equipment for the wet-spinning of refractory ceramics (such as aluminium oxide); d. Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms specified in entry I.9A.026. Note: I.1A.007.d. includes rollers, tension stretchers, coating equipment, cutting equipment and clicker dies. |
| I.1A.008 | 1B102 | Metal powder ‘ production equipment ’ and components as follows: N.B.: See also I.1A.009.b. a. Metal powder ‘ production equipment ’ usable for the ‘ production ’ , in a controlled environment, of spherical or atomised materials specified in I.1A.025.a., I.1A.025.b., I.1A.029.a.1., I.1A.029.a.2. or in the Military Goods Controls. b. Specially designed components for ‘ production equipment ’ specified in I.1A.008.a. Note: I.1A.008 includes: a. Plasma generators (high frequency arc-jet) usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment; b. Electroburst equipment usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment; c. Equipment usable for the ‘ production ’ of spherical aluminium powders by powdering a melt in an inert medium (e.g. nitrogen). |
| I.1A.009 | 1B115 | Equipment, other than that specified in I.1A.008, 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 I.1A.025.a., I.1A.025.b., I.1A.029 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 I.1A.025.a., I.1A.025.b., I.1A.029 or in the Military Goods Controls. Note: I.1A.009.b. does not prohibit batch mixers, continuous mixers or fluid energy mills. For the prohibition of batch mixers, continuous mixers and fluid energy mills see I.1A.011, I.1A.012 and I.1A.013. Note 1: For equipment specially designed for the production of military goods, see the Military Goods Controls. Note 2: I.1A.009 does not prohibit equipment for the ‘production’, handling and acceptance testing of boron carbide |
| I.1A.010 | 1B116 | 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. |
| I.1A.011 | 1B117 | 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: a. A total volumetric capacity of 110 litres or more; and b. At least one mixing/kneading shaft mounted off centre. |
| I.1A.012 | 1B118 | 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: a. Two or more mixing/kneading shafts; or b. A single rotating shaft which oscillates and having kneading teeth/pins on the shaft as well as inside the casing of the mixing chamber. |
| I.1A.013 | 1B119 | Fluid energy mills usable for grinding or milling substances specified in I.1A.025.a., I.1A.025.b., I.1A.029 or in the Military Goods Controls, and specially designed components therefore. |
| I.1A.014 | 1B201 | Filament winding machines, other than those specified in I.1A.006 or I.1A.007, and related equipment, as follows: a. Filament winding machines having all of the following characteristics: 1. Having motions for positioning, wrapping, and winding fibres coordinated and programmed in two or more axes; 2. Specially designed to fabricate composite structures or laminates from ‘ fibrous or filamentary materials ’ ; and 3. Capable of winding cylindrical rotors of diameter between 75 and 400 mm and lengths of 600 mm or greater; b. Coordinating and programming controls for the filament winding machines specified in I.1A.014.a.; c. Precision mandrels for the filament winding machines specified in I.1A.014.a. |
| I.1A.015 | 1B225 | Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour. |
| I.1A.016 | 1B226 | Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater. Note: I.1A.016 includes separators: a. Capable of enriching stable isotopes; b. With the ion sources and collectors both in the magnetic field and those configurations in which they are external to the field. |
| I.1A.017 | 1B227 | 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 |
| I.1A.018 | 1B228 | Hydrogen-cryogenic distillation columns having all of the following characteristics: a. Designed for operation with internal temperatures of 35 K (– 238 °C) or less; b. Designed for operation at an internal pressure of 0,5 to 5 MPa; c. 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; or 2. Equivalent materials which are both cryogenic and H 2 -compatible; and d. With internal diameters of 1 m or greater and effective lengths of 5 m or greater. |
| I.1A.019 | 1B229 | Water-hydrogen sulphide exchange tray columns and ‘ internal contactors ’ , as follows: N.B.: For columns which are specially designed or prepared for the production of heavy water see I.0A.005. a. Water-hydrogen sulphide exchange tray columns, having all of the following characteristics: 1. Can operate at pressures of 2 MPa or greater; 2. Constructed of carbon steel having an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; and 3. With a diameter of 1,8 m or greater; b. ‘ Internal contactors ’ for the water-hydrogen sulphide exchange tray columns specified in I.1A.019.a. Technical 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 |
| I.1A.020 | 1B230 | Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH 2 /NH 3 ), having all of the following characteristics: a. Airtight (i.e., hermetically sealed); b. A capacity greater than 8,5 m 3 /h; and c. 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 of 20 to 60 MPa. |
| I.1A.021 | 1B231 | Tritium facilities or plants, and equipment therefor, as follows: a. Facilities or plants for the production, recovery, extraction, concentration, or handling of tritium; b. Equipment for tritium facilities or plants, as follows: 1. Hydrogen or helium refrigeration units capable of cooling to 23 K (– 250 °C) or less, with heat removal capacity greater than 150 W; 2. Hydrogen isotope storage or purification systems using metal hydrides as the storage or purification medium. |
| I.1A.022 | 1B232 | 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 1 000 kg/h or greater. |
| I.1A.023 | 1B233 | 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. |
| I.1A.024 | 1C010.b | ‘ Fibrous or filamentary materials ’ which may be used in organic ‘ matrix ’ , metallic ‘ matrix ’ or carbon ‘ matrix ’ ‘ composite • structures or laminates, as follows: N.B.: See also I.1A.034 and I.9A.026. b. Carbon ‘ fibrous or filamentary materials ’ , having all of the following: 1. A ‘specific modulus’ exceeding 12,7 × 10 6 m; and 2. A ‘specific tensile strength’ exceeding 23,5 × 10 4 m; Note: I.1A.024.b. does not prohibit fabric made from ‘fibrous or filamentary materials’ for the repair of ‘civil aircraft’ structures or laminates, in which the size of individual sheets does not exceed 100 cm × 100 cm. Technical Note:Properties for materials described in I.1A.024.b. should be determined using SACMA recommended methods SRM 12 to 17, or national equivalent tow tests, such as Japanese Industrial Standard JIS-R-7601, Paragraph 6.6.2., and based on lot average. |
| I.1A.025 | 1C011.a and 1C011.b | Metals and compounds, as follows: N.B.: See also Military Goods Controls and I.1A.029. a. Metals in particle sizes of less than 60 μm whether spherical, atomised, spheroidal, flaked or ground, manufactured from material consisting of 99 % or more of zirconium, magnesium and alloys of these; Technical Note:The natural content of hafnium in the zirconium (typically 2 % to 7 %) is counted with the zirconium. Note: The metals or alloys listed in I.1A.025.a. are prohibited whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium. b. Boron or boron carbide of 85 % purity or higher and a particle size of 60 μm or less; Note: The metals or alloys listed in I.1A.025.b. are prohibited whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium. |
| I.1A.026 | 1C101 | Materials and devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures, usable in ‘ missiles ’ , ‘ missile ’ subsystems or unmanned aerial vehicles specified in I.9A.003. Note 1: I.1A.026 includes: a. Structural materials and coatings specially designed for reduced radar reflectivity; b. Coatings, including paints, specially designed for reduced or tailored reflectivity or emissivity in the microwave, infrared or ultra violet regions of the electromagnetic spectrum. Note 2: I.1A.026 does not include coatings when specially used for the thermal control of satellites. Technical Note:In I.1A.026 ‘ missile ’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km |
| I.1A.027 | 1C102 | Resaturated pyrolized carbon-carbon materials designed for space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005. N.B.: See also Military Goods Controls for materials for rockets and missiles. |
| I.1A.028 | ex 1C107* (1C107.a, ex 1C107.b, ex 1C107.c and ex 1C107.d) | Graphite and ceramic materials as follows:
|
| I.1A.029 | ex 1C111* (1C111.a.1-3, 1C111.a.4, 1C111.b.1-4 and 1C111.c) | Propellants and constituent chemicals for propellants, other than those specified in I.1A.025, as follows:
Note: For propellants and constituent chemicals for propellants not specified in I.1A.029, see the Military Goods Controls. |
| I.1A.030 | 1C116 | Maraging steels (steels generally characterised by high nickel, very low carbon content and the use of substitutional elements or precipitates to produce age-hardening) having an ultimate tensile strength of 1 500 MPa or greater, measured at 293 K (20 °C), in the form of sheet, plate or tubing with a wall or plate thickness equal to or less than 5 mm. N.B.: See also I.1A.035. |
| I.1A.031 | ex 1C117* | Tungsten, molybdenum and alloys of these metals in the form of uniform spherical or atomized particles of 500 micrometre diameter or less with a purity of 97 % or greater for fabrication of motor components, usable in ‘ missiles ’ (i.e., heat shields, nozzle substrates, nozzle throats and thrust vector control surfaces). |
| I.1A.032 | 1C118 | Titanium-stabilised duplex stainless steel (Ti-DSS) having all of the following: a. Having all of the following characteristics: 1. Containing 17,0-23,0 weight percent chromium and 4,5-7,0 weight percent nickel; 2. Having a titanium content of greater than 0,10 weight percent; and 3. A ferritic-austenitic microstructure (also referred to as a two-phase microstructure ) of which at least 10 percent is austenite by volume (according to ASTM E-1181-87 or national equivalents); and b. Having any of the following forms: 1. Ingots or bars having a size of 100 mm or more in each dimension; 2. Sheets having a width of 600 mm or more and a thickness of 3 mm or less; or 3. Tubes having an outer diameter of 600 mm or more and a wall thickness of 3 mm or less. |
| I.1A.033 | 1C202 | Alloys as follows: a. Aluminium alloys having both of the following characteristics: 1. ‘ Capable of ’ an ultimate tensile strength of 460 MPa or more at 293 K (20 °C); and 2. In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm; b. Titanium alloys having both of the following characteristics: 1. ‘ Capable of ’ an ultimate tensile strength of 900 MPa or more at 293 K (20 °C); and 2. In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm. Technical Note:The phrase alloys ‘ capable of ’ encompasses alloys before or after heat treatment. |
| I.1A.034 | 1C210 and ex 1C010.a | ‘ Fibrous or filamentary materials ’ or prepregs, other than those specified in I.1A.024, as follows: a. Carbon or aramid fibrous ‘ or filamentary materials ’ having either of the following characteristics: 1. A ‘specific modulus’ of 12,7 × 10 6 m or greater; or 2. A ‘specific tensile strength’ of 235 × 10 3 m or greater; Note: I.1A.034.a. does not prohibit aramid ‘fibrous or filamentary materials’ having 0.25 percent or more by weight of an ester based fibre surface modifier; b. Glass ‘ fibrous or filamentary materials ’ having both of the following characteristics: 1. A ‘specific modulus’ of 3,18 × 10 6 m or greater; and 2. A ‘specific tensile strength’ of 76,2 × 10 3 m or greater; Note: In I.1A.034, ‘fibrous or filamentary materials’ is restricted to continuous ‘monofilaments’, ‘yarns’, ‘rovings’, ‘tows’ or ‘tapes’. |
| I.1A.035 | 1C216 | Maraging steel, other than that specified in I.1A.030, ‘ capable of ’ an ultimate tensile strength of 2 050 MPa or more, at 293 K (20 °C). Note: I.1A.035 does not prohibit forms in which all linear dimensions are 75 mm or less. Technical Note:The phrase maraging steel ‘ capable of ’ encompasses maraging steel before or after heat treatment. |
| I.1A.036 | 1C225 | Boron enriched in the boron-10 ( 10 B) 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. Note: In I.1A.036 mixtures containing boron include boron loaded materials. Technical Note:The natural isotopic abundance of boron-10 is approximately 18,5 weight per cent (20 atom per cent). |
| I.1A.037 | 1C226 | 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. Note: I.1A.037 does not prohibit manufactures specially designed as weights or gamma ray collimators |
| I.1A.038 | 1C227 | Calcium having both of the following characteristics: a. Containing less than 1 000 parts per million by weight of metallic impurities other than magnesium; and b. Containing less than 10 parts per million by weight of boron. |
| I.1A.039 | 1C228 | Magnesium having both of the following characteristics: a. Containing less than 200 parts per million by weight of metallic impurities other than calcium; and b. Containing less than 10 parts per million by weight of boron. |
| I.1A.040 | 1C229 | Bismuth having both of the following characteristics: a. A purity of 99,99 % or greater by weight; and b. Containing less than 10 parts per million by weight of silver. |
| I.1A.041 | 1C230 | Beryllium metal, alloys containing more than 50 % beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing. Note: I.1A.041 does not prohibit the following: a. Metal windows for X-ray machines, or for bore-hole logging devices; b. Oxide shapes in fabricated or semi-fabricated forms specially designed for electronic component parts or as substrates for electronic circuits; c. Beryl (silicate of beryllium and aluminium) in the form of emeralds or aquamarines. |
| I.1A.042 | 1C231 | 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. |
| I.1A.043 | 1C232 | Helium-3 ( 3 He), mixtures containing helium-3, and products or devices containing any of the foregoing. Note: I.1A.043 does not prohibit a product or device containing less than 1 g of helium-3. |
| I.1A.044 | 1C233 | Lithium enriched in the lithium-6 ( 6 Li) 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. Note: I.1A.044 does not prohibit thermoluminescent dosimeters. Technical Note:The natural isotopic abundance of lithium-6 is approximately 6,5 weight per cent (7,5 atom per cent). |
| I.1A.045 | 1C234 | 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. Note: I.1A.045 does not prohibit zirconium in the form of foil having a thickness of 0,10 mm or less. |
| I.1A.046 | 1C235 | Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1 000 , and products or devices containing any of the foregoing. Note: I.1A.046 does not prohibit a product or device containing less than 1,48 × 10 3 GBq (40 Ci) of tritium. |
| I.1A.047 | 1C236 | 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; d. Products or devices containing any of the foregoing. Note: I.1A.047 does not prohibit a product or device containing less than 3,7 GBq (100 millicuries) of alpha activity. |
| I.1A.048 | 1C237 | Radium-226 ( 226 Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium-226, manufactures therof, and products or devices containing any of the foregoing. Note: I.1A.048 does not prohibit the following: a. Medical applicators; b. A product or device containing less than 0,37 GBq (10 millicuries) of radium-226. |
| I.1A.049 | 1C238 | Chlorine trifluoride (ClF 3 ). |
| I.1A.050 | 1C239 | High explosives, other than those specified in the Military Goods Controls, or substances or mixtures containing more than 2 % by weight thereof, with a crystal density greater than 1,8 g/cm 3 and having a detonation velocity greater than 8 000 m/s. |
| I.1A.051 | 1C240 | Nickel powder and porous nickel metal, other than those specified in I.0A.013, as follows: a. Nickel powder having both of the following characteristics: 1. A nickel purity content of 99,0 % or greater by weight; and 2. 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 I.1A.051.a. Note: I.1A.051 does not prohibit the following: a. Filamentary nickel powders; b. Single porous nickel sheets with an area of 1 000 cm 2 per sheet or less. Technical Note:I.1A.051.b. refers to porous metal formed by compacting and sintering the materials in I.1A.051.a. to form a metal material with fine pores interconnected throughout the structure. |
| I.1A.052 | ex 1C350* (1C350.1-57 and 1C350.59) | Chemicals, which may be used as precursors for toxic chemical agents, as follows, and ‘ chemical mixtures ’ containing one or more thereof: N.B.: See also Military Goods Controls and I.1A.057. 1. Thiodiglycol (111-48-8); 2. Phosphorus oxychloride (10025-87-3); 3. Dimethyl methylphosphonate (756-79-6); N.B.: See Military Goods Controls for methyl phosphonyl difluoride (676-99-3); 5. Methyl phosphonyl dichloride (676-97-1); 6. Dimethyl phosphite (DMP) (868-85-9); 7. Phosphorus trichloride (7719-12-2); 8. Trimethyl phosphite (TMP) (121-45-9); 9. Thionyl chloride (7719-09-7); 10. 3-Hydroxy-1-methylpiperidine (3554-74-3); 11. N,N-Diisopropyl-(beta)-aminoethyl chloride (96-79-7); 12. N,N-Diisopropyl-(beta)-aminoethane thiol (5842-07-9); 13. 3-Quinuclidinol (1619-34-7); 14. Potassium fluoride (7789-23-3); 15. 2-Chloroethanol (107-07-3); 16. Dimethylamine (124-40-3); 17. Diethyl ethylphosphonate (78-38-6); 18. Diethyl-N,N-dimethylphosphoramidate (2404-03-7); 19. Diethyl phosphite (762-04-9); 20. Dimethylamine hydrochloride (506-59-2); 21. Ethyl phosphinyl dichloride (1498-40-4); 22. Ethyl phosphonyl dichloride (1066-50-8); N.B.: See Military Goods Controls for ethyl phosphonyl difluoride (753-98-0); 24. Hydrogen fluoride (7664-39-3); 25. Methyl benzilate (76-89-1); 26. Methyl phosphinyl dichloride (676-83-5); 27. N,N-Diisopropyl-(beta)-amino ethanol (96-80-0); 28. Pinacolyl alcohol (464-07-3); N.B.: See Military Goods Controls for O-Ethyl-2-diisopropylaminoethyl methyl phosphonite (QL) (57856-11-8); 30. Triethyl phosphite (122-52-1); 31. Arsenic trichloride (7784-34-1); 32. Benzilic acid (76-93-7); 33. Diethyl methylphosphonite (15715-41-0); 34. Dimethyl ethylphosphonate (6163-75-3); 35. Ethyl phosphinyl difluoride (430-78-4); 36. Methyl phosphinyl difluoride (753-59-3); 37. 3-Quinuclidone (3731-38-2); 38. Phosphorus pentachloride (10026-13-8); 39. Pinacolone (75-97-8); 40. Potassium cyanide (151-50-8); 41. Potassium bifluoride (7789-29-9); 42. Ammonium hydrogen fluoride or ammonium bifluoride (1341-49-7); 43. Sodium fluoride (7681-49-4); 44. Sodium bifluoride (1333-83-1); 45. Sodium cyanide (143-33-9); 46. Triethanolamine (102-71-6); 47. Phosphorus pentasulphide (1314-80-3); 48. Di-isopropylamine (108-18-9); 49. Diethylaminoethanol (100-37-8); 50. Sodium sulphide (1313-82-2); 51. Sulphur monochloride (10025-67-9); 52. Sulphur dichloride (10545-99-0); 53. Triethanolamine hydrochloride (637-39-8); 54. N,N-Diisopropyl-(Beta)-aminoethyl chloride hydrochloride (4261-68-1); 55. Methylphosphonic acid (993-13-5); 56. Diethyl methylphosphonate (683-08-9); 57. N,N-Dimethylaminophosphoryl dichloride (677-43-0); 59. Ethyldiethanolamine (139-87-7); 63. Methylphosphonothioic dichloride (676-98-2). Note 1: I.1A.052 does not prohibit ‘chemical mixtures’ containing one or more of the chemicals specified in entries I.1A.052.1, .3, .5, .11, .12, .13, .17, .18, .21, .22, .26, .27, .28, .31, .32, .33, .34, .35, .36, .54, .55, .56, .57 and .63 in which no individually specified chemical constitutes more than 10 % by the weight of the mixture. Note 2: I.1A.052 does not prohibit ‘chemical mixtures’ containing one or more of the chemicals specified in entries I.1A.052 .2, .6, .7, .8, .9, .10, .14, .15, .16, .19, .20, .24, .25, .30, .37, .38, .39, .40, .41, .42, .43, .44, .45, .46, .47, .48, .49, .50, .51, .52, .53 and .59 in which no individually specified chemical constitutes more than 30 % by the weight of the mixture. Note 3: I.1A.052 does not prohibit products identified as consumer goods packaged for retail sale for personal use or packaged for individual use. |
| I.1A.053 | ex 1C351* (1C351.a.1-28, 1C351.b, 1C351.c, 1C351.d.1-8, ex 1C351.d.9, 1C351.d.10-13 and 1C351.d.15-16) | Human pathogens, zoonoses and ‘ toxins ’ , as follows:
Note: I.1A.053 does not prohibit ‘vaccines’ or ‘immunotoxins’. |
| I.1A.054 | ex 1C352* (1C352.a.1-15 and 1C352.b.1) | Animal pathogens, as follows:
Note: I.1A.054 does not prohibit ‘vaccines’. |
| I.1A.055 | ex 1C353* ( ex 1C353.a, 1C353.b) | Genetic elements and genetically modified organisms, as follows:
Technical Notes:1. Genetic elements include, inter alia, chromosomes, genomes, plasmids, transposons and vectors whether genetically modified or unmodified.2. Nucleic acid sequences associated with the pathogenicity of any of the micro-organisms specified in I.1A.053.a. to c. or I.1A.054 or I.1A.056 means any sequence specific to the specified micro-organism that:a. In itself or through its transcribed or translated products represents a significant hazard to human, animal or plant health; or b. Is known to enhance the ability of a specified micro-organism, or any other organism into which it may be inserted or otherwise integrated, to cause serious harm to humans, animals or plant health. Note: I.1A.055 does not apply to nucleic acid sequences associated with the pathogenicity of enterohaemorrhagic Escherichia coli, serotype O157 and other verotoxin producing strains, other than those coding for the verotoxin, or for its sub-units. |
| I.1A.056 | ex 1C354* (1C354.b.1-3 and 1C354.c) | Plant pathogens, as follows:
|
| I.1A.057 | 1C450 | Toxic chemicals and toxic chemical precursors, as follows, and ‘ chemical mixtures ’ containing one or more thereof: N.B.: See also entry I.1A.052, I.1A.053.d. and Military Goods Controls.
|
| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|---|---|
| I.1B.001 | ex 1D001 | ‘ Software ’ specially designed or modified for the ‘ development ’ , ‘ production ’ or ‘ use ’ of equipment specified in I.1A.006. |
| I.1B.002 | 1D101 | ‘ Software ’ specially designed or modified for the ‘ use ’ of goods specified in I.1A.007 to I.1A.009, or I.1A.011 to I.1A.013. |
| I.1B.003 | 1D103 | ‘ Software ’ specially designed for analysis of reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures. |
| I.1B.004 | 1D201 | ‘ Software ’ specially designed for the ‘ use ’ of goods specified in I.1A.014. |
| I.1B.005 | 1E001 | ‘ Technology ’ according to the General Technology Note for the ‘ development ’ or ‘ production ’ of equipment or materials specified in I.1A.006 to I.1A.053, I.1A.055 or I.1A.057. |
| I.1B.006 | 1E101 | ‘ Technology ’ according to the General Technology Note for the ‘ use ’ of goods specified in I.1A.001, I.1A.006 to I.1A.013 I.1A.026, I.1A.028, I.1A.029 to I.1A.032, I.1B.002 or I.1B.003. |
| I.1B.007 | ex 1E102 | ‘ Technology ’ according to the General Technology Note for the ‘ development ’ of ‘ software ’ specified in I.1B.001to I.1B.003. |
| I.1B.008 | 1E103 | ‘ Technology ’ for the regulation of temperature, pressure or atmosphere in autoclaves or hydroclaves, when used for the ‘ production ’ of ‘ composites ’ or partially processed ‘ composites ’ . |
| I.1B.009 | 1E104 | ‘ Technology ’ relating to the ‘ production ’ of pyrolytically 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. Note: I.1B.009 includes ‘technology’ for the composition of precursor gases, flow-rates and process control schedules and parameters. |
| I.1B.010 | ex 1E201 | ‘ Technology ’ according to the General Technology Note for the ‘ use ’ of goods specified in I.1A.002 to I.1A.005, I.1A.014 to I.1A.023, I.1A.024.b., I.1A.033 to I.1A.051, or I.1B.004. |
| I.1B.011 | 1E202 | ‘ Technology ’ according to the General Technology Note for the ‘ development ’ or ‘ production ’ of goods specified in I.1A.002 to I.1A.005. |
| I.1B.012 | 1E203 | ‘ Technology ’ according to the General Technology Note for the ‘ development ’ of ‘ software ’ specified in I.1B.004. |
| a Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of the Member State in which they are established. | ||
| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|---|---|
| I.2A.001 | ex 2A001* | Anti-friction bearings and bearing systems, as follows, and components therefor: Note: I.2A.001 does not prohibit balls with tolerances specified by the manufacturer in accordance with ISO 3290 as grade 5 or worse. Radial ball 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 and having all of the following characteristics: a. An inner ring bore diameter between 12 and 50 mm; b. An outer ring outside diameter between 25 and 100 mm; and c. A width between 10 and 20 mm. |
| I.2A.002 | 2A225 | Crucibles made of materials resistant to liquid actinide metals, as follows: a. Crucibles having both of the following characteristics: 1. A volume of between 150 cm 3 and 8 000 cm 3 ; and 2. Made of or coated with any of the following materials, having a purity of 98 % or greater by weight: a. Calcium fluoride (CaF 2 ); b. Calcium zirconate (metazirconate) (CaZrO 3 ); c. Cerium sulphide (Ce 2 S 3 ); d. Erbium oxide (erbia) (Er 2 O 3 ); e. Hafnium oxide (hafnia) (HfO 2 ); f. Magnesium oxide (MgO); g. Nitrided niobium-titanium-tungsten alloy (approximately 50 % Nb, 30 % Ti, 20 % W); h. Yttrium oxide (yttria) (Y 2 O 3 ); or i. Zirconium oxide (zirconia) (ZrO 2 ); b. Crucibles having both of the following characteristics: 1. A volume of between 50 cm 3 and 2 000 cm 3 ; and 2. Made of or lined with tantalum, having a purity of 99,9 % or greater by weight; c. Crucibles having all of the following characteristics: 1. A volume of between 50 cm 3 and 2 000 cm 3 ; 2. Made of or lined with tantalum, having a purity of 98 % or greater by weight; and 3. Coated with tantalum carbide, nitride, boride, or any combination thereof |
| I.2A.003 | 2A226 | Valves having all of the following characteristics: a. A ‘ nominal size ’ of 5 mm or greater; b. Having a bellows seal; and c. Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60 % nickel by weight. Technical Note:For valves with different inlet and outlet diameters, the ‘ nominal size ’ in I.2A.003 refers to the smallest diameter |
| I.2A.004 | ex 2B001.a*, 2B001.d | Machine tools and any combination thereof, for removing (or cutting) metals, ceramics or ‘ composites ’ , which, according to the manufacturer’s technical specification, can be equipped with electronic devices for ‘ numerical control ’ , and specially designed components as follows: N.B.: See also I.2A.016. Note 1: I.2A.004 does not prohibit special purpose machine tools limited to the manufacture of gears. Note 2: I.2A.004 does not prohibit special purpose machine tools limited to the manufacture of any of the following parts: a. Crankshafts or camshafts; b. Tools or cutters; c. Extruder worms; Note 3: A machine tool having at least two of the three turning, milling or grinding capabilities (e.g., a turning machine with milling capability), must be evaluated against each applicable entry I.2A.004.a and I.2A.016.
|
| I.2A.005 | ex 2B006.b* | Dimensional inspection or measuring systems, equipment and ‘ electronic assemblies ’ , as follows:
|
| I.2A.006 | 2B007.c | ‘ Robots ’ having the following characteristics and specially designed controllers and ‘ end-effectors ’ therefor: N.B.: See also I.2A.019. c. Specially designed or rated as radiation-hardened to withstand a total radiation dose greater than 5 × 10 3 Gy (silicon) without operational degradation. Technical Note:The term Gy (silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionising radiation. |
| I.2A.007 | 2B104 | ‘ Isostatic presses ’ having all of the following: N.B.: See also I.2A.017. a. Maximum working pressure of 69 MPa or greater; b. Designed to achieve and maintain a controlled thermal environment of 873 K (600 °C) or greater; and c. Possessing a chamber cavity with an inside diameter of 254 mm or greater. |
| I.2A.008 | 2B105 | Chemical vapour deposition (CVD) furnaces designed or modified for the densification of carbon-carbon composites. |
| I.2A.009 | 2B109 | Flow-forming machines and specially designed components as follows: N.B.: See also I.2A.020. a. Flow-forming machines having all of the following: 1. 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; and 2. With more than two axes which can be coordinated simultaneously for ‘ contouring control ’ . b. Specially designed components for flow-forming machines specified in I.2A.009.a. Note: I.2A.009 does not prohibit machines that are not usable in the production of propulsion components and equipment (e.g. motor cases) for ‘missiles’. Technical Note:Machines combining the function of spin-forming and flow-forming are for the purpose of I.2A.009 regarded as flow-forming machines |
| I.2A.010 | 2B116 | Vibration test systems, equipment and components therefor, as follows: a. 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 ’ ; b. 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 I.2A.010.a.; c. 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 I.2A.010.a.; d. 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 I.2A.010.a. Technical Note:In I.2A.010, ‘ bare table ’ means a flat table, or surface, with no fixture or fittings |
| I.2A.011 | 2B117 | Equipment and process controls, other than those specified in I.2A.007 or I.2A.008, designed or modified for densification and pyrolysis of structural composite rocket nozzles and reentry vehicle nose tips. |
| I.2A.012 | 2B119 | Balancing machines and related equipment, as follows: N.B.: See also I.2A.021. a. Balancing machines having all the following characteristics: 1. Not capable of balancing rotors/assemblies having a mass greater than 3 kg; 2. Capable of balancing rotors/assemblies at speeds greater than 12 500 rpm; 3. Capable of correcting unbalance in two planes or more; and 4. Capable of balancing to a residual specific unbalance of 0,2 g mm per kg of rotor mass; Note: I.2A.012.a. does not prohibit balancing machines designed or modified for dental or other medical equipment. |
| I.2A.013 | 2B120 | Motion simulators or rate tables having all of the following characteristics: a. Two axes or more; b. Slip rings capable of transmitting electrical power and/or signal information; and c. Having any of the following characteristics: 1. For any single axis having all of the following: a. Capable of rates of 400 degrees/s or more, or 30 degrees/s or less; and b. A rate resolution equal to or less than 6 degrees/s and an accuracy equal to or less than 0,6 degrees/s; 2. Having a worst-case rate stability equal to or better (less) than plus or minus 0,05 % averaged over 10 degrees or more; or 3. A positioning accuracy equal to or better than 5 arc second. Note: I.2A.013 does not prohibit rotary tables designed or modified for machine tools or for medical equipment. |
| I.2A.014 | 2B121 | Positioning tables (equipment capable of precise rotary positioning in any axes), other than those specified in I.2A.013, having all the following characteristics: a. Two axes or more; and b. A positioning accuracy equal to or better than 5 arc second. Note: I.2A.014 does not prohibit rotary tables designed or modified for machine tools or for medical equipment. |
| I.2A.015 | 2B122 | Centrifuges capable of imparting accelerations above 100 g and having slip rings capable of transmitting electrical power and signal information. |
| I.2A.016 | 2B201, 2B001.b.2 and 2B001.c.2 | Machine tools and any combination thereof, as follows, for removing or cutting metals, ceramics or ‘ composites ’ , which, according to the manufacturer’s technical specification, can be equipped with electronic devices for simultaneous ‘ contouring control ’ in two or more axes: Note: For ‘numerical control’ units prohibited because of their associated ‘software’ see I.2B.002. a. Machine tools for milling, having any of the following characteristics: 1. Positioning accuracies with ‘all compensations available’ equal to or less (better) than 6 μm according to ISO 230/2 (1988) a or national equivalents along any linear axis; 2. Two or more contouring rotary axes; or 3. Five or more axes which can be coordinated simultaneously for ‘ contouring control ’ . Note: I.2A.016.a. does not prohibit milling machines having the following characteristics: a. X-axis travel greater than 2 m; and b. Overall positioning accuracy on the x-axis more (worse) than 30 μm. b. Machine tools for grinding, having any of the following characteristics: 1. Positioning accuracies with ‘all compensations available’ equal to or less (better) than 4 μm according to ISO 230/2 (1988) a or national equivalents along any linear axis; 2. Two or more contouring rotary axes; or 3. Five or more axes which can be coordinated simultaneously for ‘ contouring control ’ . Note: I.2A.016.b. does not prohibit the following grinding machines: a. Cylindrical external, internal, and external-internal grinding machines having all of the following characteristics: 1. Limited to a maximum workpiece capacity of 150 mm outside diameter or length; and 2. Axes limited to x, z and c; b. Jig grinders that do not have a z-axis or a w-axis with an overall positioning accuracy less (better) than 4 μm according to ISO 230/2 (1988) a or national equivalents. Note 1: I.2A.016 does not prohibit special purpose machine tools limited to the manufacture of any of the following parts: a. Gears; b. Crankshafts or camshafts; c. Tools or cutters; d. Extruder worms. Note 2: A machine tool having at least two of the three turning, milling or grinding capabilities (e.g., a turning machine with milling capability), must be evaluated against each applicable entry I.2A.004.a. or I.2A.016.a. or b. |
| I.2A.017 | 2B204 | ‘ Isostatic presses ’ , other than those specified in I.2A.007, and related equipment, as follows: a. ‘ Isostatic presses ’ having both of the following characteristics: 1. Capable of achieving a maximum working pressure of 69 MPa or greater; and 2. A chamber cavity with an inside diameter in excess of 152 mm; b. Dies, moulds and controls, specially designed for ‘ isostatic presses ’ specified in I.2A.017.a. Technical Note:In I.2A.017 the inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other. |
| I.2A.018 | 2B206 | Dimensional inspection machines, instruments or systems, other than those specified in I.2A.005, as follows: a. Computer controlled or numerically controlled dimensional inspection machines having both of the following characteristics: 1. Two or more axes; and 2. A one-dimensional length ‘ measurement uncertainty ’ equal to or less (better) than (1,25 + L/ 1 000 ) μm tested with a probe of an ‘ accuracy ’ of less (better) than 0,2 μm (L is the measured length in millimetres) (Ref.: VDI/VDE 2617 Parts 1 and 2); b. Systems for simultaneous linear-angular inspection of hemishells, having both of the following characteristics: 1. ‘ Measurement uncertainty ’ along any linear axis equal to or less (better) than 3,5 μm per 5 mm; and 2. ‘ Angular position deviation ’ equal to or less than 0,02 °. Note 1: Machine tools that can be used as measuring machines are prohibited if they meet or exceed the criteria specified for the machine tool function or the measuring machine function. Note 2: A machine specified in I.2A.018 is prohibited if it exceeds the prohibition threshold anywhere within its operating range. Technical 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 4.2. All parameters of measurement values in I.2A.018 represent plus/minus i.e., not total band. |
| I.2A.019 | 2B207 | ‘ Robots ’ , ‘ end effectors ’ and control units, other than those specified in I.2A.006, as follows: a. ‘ 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); b. Control units specially designed for any of the ‘ robots ’ or ‘ end effectors ’ specified in I.2A.019.a. |
| I.2A.020 | 2B209 | Flow forming machines, spin forming machines capable of flow forming functions, other than those specified in I.2A.009, and mandrels, as follows: a. Machines having both of the following characteristics: 1. Three or more rollers (active or guiding); and 2. Which, according to the manufacturer's technical specification, can be equipped with ‘ numerical control ’ units or a computer control; b. Rotor-forming mandrels designed to form cylindrical rotors of inside diameter between 75 mm and 400 mm. Note: I.2A.020.a. includes machines which have only a single roller designed to deform metal plus two auxiliary rollers which support the mandrel, but do not participate directly in the deformation process. |
| I.2A.021 | 2B219 | Centrifugal multiplane balancing machines, fixed or portable, horizontal or vertical, as follows: a. Centrifugal balancing machines designed for balancing flexible rotors having a length of 600 mm or more and having all of the following characteristics: 1. Swing or journal diameter greater than 75 mm; 2. Mass capability of from 0,9 to 23 kg; and 3. Capable of balancing speed of revolution greater than 5 000 r.p.m.; b. Centrifugal balancing machines designed for balancing hollow cylindrical rotor components and having all of the following characteristics: 1. Journal diameter greater than 75 mm; 2. Mass capability of from 0,9 to 23 kg; 3. Capable of balancing to a residual imbalance equal to or less than 0,01 kg × mm/kg per plane; and 4. Belt drive type. |
| I.2A.022 | 2B225 | 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); or b. 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). Technical Note:Remote manipulators provide translation of human operator actions to a remote operating arm and terminal fixture. They may be of ‘ master/slave ’ type or operated by joystick or keypad. |
| I.2A.023 | 2B226 | Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows: a. Furnaces having all of the following characteristics: 1. Capable of operation above 1 123 K (850 °C); 2. Induction coils 600 mm or less in diameter; and 3. Designed for power inputs of 5 kW or more; b. Power supplies, with a specified power output of 5 kW or more, specially designed for furnaces specified in I.2A.023.a. Note: I.2A.023.a. does not prohibit furnaces designed for the processing of semiconductor wafers. |
| I.2A.024 | 2B227 | 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 cm 3 and 20 000 cm 3 , and 2. Capable of operating with melting temperatures above 1 973 K ( 1 700 °C); b. Electron beam melting furnaces and plasma atomization and melting furnaces, having both of the following characteristics: 1. A power of 50 kW or greater; and 2. Capable of operating with melting temperatures above 1 473 K ( 1 200 °C). c. Computer control and monitoring systems specially configured for any of the furnaces specified in I.2A.024.a. or b. |
| I.2A.025 | 2B228 | Rotor fabrication or assembly equipment, rotor straightening equipment, bellows forming mandrels and dies, as follows: a. Rotor assembly equipment for assembly of gas centrifuge rotor tube sections, baffles, and end caps; Note: I.2A.025.a. includes precision mandrels, clamps, and shrink fit machines. b. Rotor straightening equipment for alignment of gas centrifuge rotor tube sections to a common axis; Technical Note:In I.2A.025.b. such equipment normally consists of precision measuring probes linked to a computer that subsequently controls the action of, for example, pneumatic rams used for aligning the rotor tube sections. c. Bellows-forming mandrels and dies for producing single convolution bellows. Technical Note:In I.2A.025.c. the bellows have all of the following characteristics: 1. Inside diameter between 75 mm and 400 mm; 2. Length equal to or greater than 12,7 mm; 3. Single convolution depth greater than 2 mm; and 4. Made of high-strength aluminium alloys, maraging steel or high strength ‘ fibrous or filamentary materials ’ . |
| I.2A.026 | 2B230 | ‘ Pressure transducers ’ capable of measuring absolute pressures at any point in the range 0 to 13 kPa and having both of the following characteristics: a. Pressure sensing elements made of or protected by aluminium, aluminium alloy, nickel or nickel alloy with more than 60 % nickel by weight; and b. Having either of the following characteristics: 1. A full scale of less than 13 kPa and an ‘ accuracy ’ of better than + 1 % of full-scale; or 2. A full scale of 13 kPa or greater and an ‘ accuracy ’ of better than + 130 Pa. Technical Note:For the purposes of I.2A.026, ‘ accuracy ’ includes non linearity, hysteresis and repeatability at ambient temperature. |
| I.2A.027 | 2B231 | 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 m 3 /s; and c. Capable of producing an ultimate vacuum better than 13 mPa. Technical Note:1. The pumping speed is determined at the measurement point with nitrogen gas or air.2. The ultimate vacuum is determined at the input of the pump with the input of the pump blocked off |
| I.2A.028 | 2B232 | 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 |
| I.2A.029 | ex 2B350* (2B350.a.1-7, ex 2B350.b.1-7, 2B350.c.1-7, ex 2B350.d.1-8, ex 2B350.e.1-8, 2B350.f, ex 2B350.g.1-7, ex 2B350.h.1-7, ex 2B350.i.1-10 and 2B350.j) | Chemical manufacturing facilities, equipment and components, as follows:
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| I.2A.030 | 2B351 | Toxic gas monitoring systems, as follows; and dedicated detectors therefor: a. Designed for continuous operation and usable for the detection of chemical warfare agents or chemicals specified in I.1A.052, at concentrations of less than 0,3 mg/m 3 ; or b. Designed for the detection of cholinesterase-inhibiting activity. |
| I.2A.031 | ex 2B352* and — (2B352.a, 2B352.b, 2B352.c, ex 2B352.d.1, ex 2B352.e, ex 2B352.f.1, 2B352.f.2 and 2B352.g) | Equipment capable of use in handling biological materials, as follows:
|
| I.2A.032 | — | Equipment capable of use in handling biological materials, other than that specified in I.2A.031, as follows: a. Equipment for the micro-encapsulation of live micro-organisms and toxins in the range of 1-10 μm particle size, as follows: 1. Interfacial polycondensors; 2. Phase separators. b. Conventional or turbulent air-flow clean-air rooms and self-contained fan-HEPA filter units that may be used for P3 or P4 (BL3, BL4, L3, L4) containment facilities. |
| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|---|---|
| I.2B.001 | ex 2D001 | ‘ Software ’ , other than that specified in I.2B.002, specially designed or modified for the ‘ development ’ , ‘ production ’ or ‘ use ’ of equipment specified in I.2A.004 to I.2A.006. |
| I.2B.002 | 2D002 | ‘ Software ’ for electronic devices, even when residing in an electronic device or system, enabling such devices or systems to function as a ‘ numerical control ’ unit, capable of co-ordinating simultaneously more than four axes for ‘ contouring control ’ . Note 1: I.2B.002 does not prohibit ‘software’ specially designed or modified for the operation of machine tools not specified in Category I.2. |
| I.2B.003 | 2D101 | ‘ Software ’ specially designed or modified for the ‘ use ’ of equipment specified in I.2A.007 to I.2A.015. |
| I.2B.004 | 2D201 | ‘ Software ’ specially designed for the ‘ use ’ of equipment specified in I.2A.017 to I.2A.024. Note: ‘Software’ specially designed for equipment specified in I.2A.018 includes ‘software’ for simultaneous measurements of wall thickness and contour |
| I.2B.005 | 2D202 | ‘ Software ’ specially designed or modified for the ‘ development ’ , ‘ production ’ or ‘ use ’ of equipment specified in I.2A.016. |
| I.2B.006 | ex 2E001 and — | ‘ Technology ’ according to the General Technology Note for the ‘ development ’ of equipment or ‘ software ’ specified in I.2A.002 to I.2A.004, I.2A.006.b., I.2A.006.c, I.2A.007 to I.2A.032, I.2B.001, I.2B.003 or I.2B.004. |
| I.2B.007 | ex 2E002 and — | ‘ Technology ’ according to the General Technology Note for the ‘ production ’ of equipment specified in I.2A.002 to I.2A.004, I.2A.006.b., I.2A.006.c, I.2A.007 to I.2A.032 |
| I.2B.008 | 2E101 | ‘ Technology ’ according to the General Technology Note for the ‘ use ’ of equipment or ‘ software ’ specified in I.2A.007, I.2A.009, I.2A.010, I.2A.012 to I.2A.015 or I.2B.003. |
| I.2B.009 | ex 2E201 | ‘ Technology ’ according to the General Technology Note for the ‘ use ’ of equipment or ‘ software ’ specified in I.2A.002 to I.2A.005, I.2A.006.b., I.2A.006.c., I.2A.016 to I.2A.020, I.2A.022 to I.2A.028, I.2B.004 or I.2B.005. |
| I.2B.010 | 2E301 | ‘ Technology ’ according to the General Technology Note for the ‘ use ’ of goods specified in I.2A.029 to I.2A.031. |
| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|---|---|
| I.3B.001 | 3D101 | ‘ Software ’ specially designed or modified for the ‘ use ’ of equipment specified in I.3A.002.b |
| I.3B.002 | ex 3E001 | ‘ Technology ’ according to the General Technology Note for the ‘ development ’ or ‘ production ’ of equipment or materials specified in I.3A.001 to I.3A.003, or in I.3A.007 to I.3A.012. |
| I.3B.003 | ex 3E101 | ‘ Technology ’ according to the General Technology Note for the ‘ use ’ of equipment or ‘ software ’ specified in I.3A.001, I.3A.002 or I.3B.001. |
| I.3B.004 | 3E102 | ‘ Technology ’ according to the General Technology Note for the ‘ development ’ of ‘ software ’ specified in I.3B.001. |
| I.3B.005 | ex 3E201 | ‘ Technology ’ according to the General Technology Note for the ‘ use ’ of equipment specified in I.3A.003 to I.3A.012. |
| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|---|---|
| I.4A.001 | 4A001.a.1 * | Electronic computers and related equipment, as follows: N.B.: See also I.4A.002. a. Specially designed to have the following characteristics:
|
| I.4A.002 | 4A101 | Analogue computers, ‘ digital computers ’ or digital differential analysers, having all of the following characteristics: N.B.: See also Military Goods Controls for computers for use in rockets or missiles. a. Designed or modified for use in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005; and b. Designed as ruggedised or radiation hardened to withstand radiation levels of 5 × 10 3 Gy (silicon) or higher. |
| I.4A.003 | 4A102 | ‘ Hybrid computers ’ specially designed for modelling, simulation or design integration of space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005. N.B.: See also Military Goods Controls for rockets or missiles related computers. Note: This prohibition only applies when the equipment is supplied with ‘software’ specified in I.7B.003 or I.9B.003. |
| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|---|---|
| I.4B.001 | ex 4E001.a | ‘ Technology ’ according to the General Technology Note, for the ‘ development ’ , ‘ production ’ or ‘ use ’ of equipment or ‘ software ’ specified in I.4A.001, I.4A.002 or I.4A.003. |
| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|---|---|
| I.5B.001 | 5D101 | ‘ Software ’ specially designed or modified for the ‘ use ’ of equipment specified in I.5A.001. |
| I.5B.002 | 5E101 | ‘ Technology ’ according to the General Technology Note for the ‘ development ’ , ‘ production ’ or ‘ use ’ of equipment specified in I.5A.001 or software specified in I.5B.001. |
| a The texts of points a, b and c in this entry do not correspond with those of points a, b and c of 6A005. | ||
| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|---|---|
| I.6A.001 | ex 6A005.b*, ex 6A005.c* and ex 6A005.d* a.: ex 6A005.d.4 b.: ex 6A005.b.2-4 c.: ex 6A005.c.2 | ‘Lasers’, other than those specified in I.0A.002.g.5. or I.0A.002.h.6., components and optical equipment, as follows: a a. Pulsed excimer (XeF, XeCl, KrF) ‘ lasers ’ having all of the following characteristics: 1. Operating at wavelengths between 240 nm and 360 nm; 2. A repetition rate greater than 250 Hz; and 3. An average output power exceeding 500 W. b. Copper (Cu) vapour ‘ lasers ’ having both of the following characteristics: 1. Operating at wavelengths between 500 nm and 600 nm; and 2. An average output power exceeding 40 W. c. Solid state ‘tunable’ alexandrite (CR: BeAl 2 O 4 ) ‘lasers’ having all of the following characteristics: 1. Operating at wavelengths between 720 nm and 800 nm; 2. A bandwidth of 0,005 nm or less; 3. A repetition rate greater than 125 Hz; and 4. An average output power exceeding 30 W. |
| I.6A.002 | 6A007.c | Gravity gradiometers. |
| I.6A.003 | 6A102 | Radiation hardened ‘detectors’ specially designed or modified for protecting against nuclear effects (e.g. electromagnetic pulse (EMP), X-rays, combined blast and thermal effects) and usable for ‘missiles’, designed or rated to withstand radiation levels which meet or exceed a total irradiation dose of 5 × 10 5 rads (silicon). Technical Note:In I.6A.003, a ‘ detector ’ is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material. This includes devices that sense by one time operation or failure. |
| I.6A.004 | 6A107 | Gravity meters (gravimeters) and components for gravity meters and gravity gradiometers, as follows: a. Gravity meters, designed or modified for airborne or marine use, and having a static or operational accuracy of 7 × 10 –6 m/s 2 (0,7 milligal) or less (better), and having a time-to-steady-state registration of two minutes or less; b. Specially designed components for gravity meters specified in I.6A.004.a. and gravity gradiometers specified in I.6A.002. |
| I.6A.005 | 6A108 | Radar systems and tracking systems as follows: a. Radar and laser radar systems designed or modified for use in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005; N.B.: See also Military Goods Controls for radar and laser systems for rockets or missiles. Note: I.6A.005.a. includes the following: a. Terrain contour mapping equipment; b. Imaging sensor equipment; c. Scene mapping and correlation (both digital and analogue) equipment; d. Doppler navigation radar equipment. b. Precision tracking systems, usable for ‘ missiles ’ , as follows: 1. Tracking systems which use a code translator in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurements of in-flight position and velocity; 2. Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities: a. Angular resolution better than 3 milliradians; b. Range of 30 km or greater with a range resolution better than 10 m rms; c. Velocity resolution better than 3 m/s. Technical Note:In I.6A.005.b. ‘ missile ’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
| I.6A.006 | 6A202 | Photomultiplier tubes having both of the following characteristics: a. Photocathode area of greater than 20 cm 2 ; and b. Anode pulse rise time of less than 1 ns. |
| I.6A.007 | 6A203 | Cameras and components, as follows: a. Mechanical rotating mirror cameras, as follows, and specially designed components therefor: 1. Framing cameras with recording rates greater than 225 000 frames per second; 2. Streak cameras with writing speeds greater than 0,5 mm per microsecond; Note: In I.6A.007.a. components of such cameras include their synchronizing electronics units and rotor assemblies consisting of turbines, mirrors and bearings. b. Electronic streak cameras, electronic framing cameras, tubes and devices, as follows: 1. Electronic streak cameras capable of 50 ns or less time resolution; 2. Streak tubes for cameras specified in I.6A.007.b.1.; 3. Electronic (or electronically shuttered) framing cameras capable of 50 ns or less frame exposure time; 4. Framing tubes and solid-state imaging devices for use with cameras specified in I.6A.007.b.3., as follows: a. Proximity focused image intensifier tubes having the photocathode deposited on a transparent conductive coating to decrease photocathode sheet resistance; b. 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; c. Kerr or Pockels cell electro-optical shuttering; d. 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 I.6A.007.b.3.; c. Radiation-hardened TV cameras, or lenses therefor, specially designed or rated as radiation hardened to withstand a total radiation dose greater than 50 × 10 3 Gy (silicon) (5 × 10 6 rad (silicon)) without operational degradation. Technical Note:The term Gy (silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionising radiation |
| I.6A.008 | 6A205 | ‘ Lasers ’ , ‘ laser ’ amplifiers and oscillators, other than those specified in I.0A.002.g.5., I.0A.002.h.6. and I.6A.001; as follows: a. Argon ion ‘ lasers ’ having both of the following characteristics: 1. Operating at wavelengths between 400 nm and 515 nm; and 2. An average output power greater than 40 W; b. Tunable pulsed single-mode dye laser oscillators having all of the following characteristics: 1. Operating at wavelengths between 300 nm and 800 nm; 2. An average output power greater than 1 W; 3. A repetition rate greater than 1 kHz; and 4. Pulse width less than 100 ns; c. Tunable pulsed dye laser amplifiers and oscillators, having all of the following characteristics: 1. Operating at wavelengths between 300 nm and 800 nm; 2. An average output power greater than 30 W; 3. A repetition rate greater than 1 kHz; and 4. Pulse width less than 100 ns; Note: I.6A.008.c. does not prohibit single mode oscillators; d. Pulsed carbon dioxide ‘ lasers ’ having all of the following characteristics: 1. Operating at wavelengths between 9 000 nm and 11 000 nm; 2. A repetition rate greater than 250 Hz; 3. An average output power greater than 500 W; and 4. Pulse width of less than 200 ns; e. Para-hydrogen Raman shifters designed to operate at 16 micrometre output wavelength and at a repetition rate greater than 250 Hz; f. Neodymium-doped (other than glass) ‘ lasers ’ , having an output wavelength exceeding 1 000 nm but not exceeding 1 100 nm, as follows: 1. Pulse-excited, ‘ Q-switched lasers ’ having a ‘ pulse duration ’ equal to or more than 1 ns, and having either of the following: a. A single-transverse mode output having an average output power exceeding 40 W; or b. A multiple-transverse mode output having an average power exceeding 50 W; or 2. Incorporating frequency doubling to give an output wavelength of 500 nm or more but not exceeding 550 nm and having an average output power exceeding 40 W. |
| I.6A.009 | 6A225 | Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 microseconds. Note: I.6A.009 includes velocity interferometers such as VISARs (Velocity interferometer systems for any reflector) and DLIs (Doppler laser interferometers). |
| I.6A.010 | 6A226 | Pressure sensors, as follows: a. Manganin gauges for pressures greater than 10 GPa; b. Quartz pressure transducers for pressures greater than 10 GPa |
| I.6A.011 | ex 6B108* | Systems specially designed for radar cross section measurement usable for ‘ missiles ’ and their subsystems. |
| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|---|---|
| I.7B.001 | ex 7D101 | ‘ Software ’ specially designed or modified for the ‘ use ’ of equipment specified in I.7A.001 to I.7A.008, I.7A.009.a., I.7A.009.b. or I.7A.011 to I.7A.015 |
| I.7B.002 | 7D102 | Integration ‘ software ’ as follows: a. Integration ‘ software ’ for the equipment specified in I.7A.004.b.; b. Integration ‘ software ’ specially designed for the equipment specified in I.7A.004.a. c. Integration ‘ software ’ designed or modified for the equipment specified in I.7A.004.c. Note: A common form of integration ‘software’ employs Kalman filtering. |
| I.7B.003 | 7D103 | ‘ Software ’ specially designed for modelling or simulation of the ‘ guidance sets ’ specified in I.7A.010 or for their design integration with the space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005. Note: ‘Software’ specified in I.7B.003 remains prohibited when combined with specially designed hardware specified in I.4A.003. |
| I.7B.004 | ex 7E001 | ‘ Technology ’ according to the General Technology Note for the ‘ development ’ of equipment or ‘ software ’ specified in I.7A.001 to I.7A.015, or in I.7B.001 to I.7B.003. |
| I.7B.005 | ex 7E002 | ‘ Technology ’ according to the General Technology Note for the ‘ production ’ of equipment specified in I.7A.001 to I.7A.015. |
| I.7B.006 | 7E101 | ‘ Technology ’ according to the General Technology Note for the ‘ use ’ of equipment specified in I.7A.001 to I.7A.015 or I.7B.001 to I.7B.003. |
| I.7B.007 | 7E102 | ‘ Technology ’ for protection of avionics and electrical subsystems against electromagnetic pulse (EMP) and electromagnetic interference (EMI) hazards, from external sources, as follows: a. Design ‘ technology ’ for shielding systems; b. Design ‘ technology ’ for the configuration of hardened electrical circuits and subsystems; c. Design ‘ technology ’ for the determination of hardening criteria of I.7B.007.a. and I.7B.007.b. |
| I.7B.008 | 7E104 | ‘ Technology ’ for the integration of the flight control, guidance, and propulsion data into a flight management system for optimization of rocket system trajectory. |
| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|---|---|
| I.9B.001 | ex 9D001 | ‘ Software ’ specially designed or modified for the ‘ development ’ of equipment or ‘ technology ’ specified in I.9A.002, I.9A.009, I.9A.012, I.9A.015 or I.9A.016. |
| I.9B.002 | 9D101 | ‘ Software ’ specially designed or modified for the ‘ use ’ of goods specified in I.9A.020, I.9A.021, I.9A.023 or I.9A.024. |
| I.9B.003 | 9D103 | ‘ Software ’ specially designed for modelling, simulation or design integration of the space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005, or the subsystems specified in I.9A.006.a., I.9A.007, I.9A.009, I.9A.014 or I.9A.017. Note: ‘Software’ specified in I.9B.003 remains prohibited when combined with specially designed hardware specified in I.4A.003. |
| I.9B.004 | ex 9D104 | ‘Software’ specially designed or modified for the ‘use’ of [X1goods specified in I.9A.002] , I.9A.004, I.9A.006, I.9A.007.c., I.9A.007.d., I.9A.008, I.9A.009.c., I.9A.010, I.9A.012, I.9A.013.a., I.9A.014.d., I.9A.015 or I.9A.016. |
| I.9B.005 | 9D105 | ‘ Software ’ which coordinates the function of more than one subsystem, specially designed or modified for ‘ use ’ in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005. |
| I.9B.006 | ex 9E001 | ‘ Technology ’ according to the General Technology Note for the ‘ development ’ of equipment or ‘ software ’ specified in I.9A.001, I.9A.003, I.9A.021 to I.9A.024, or I.9B.002 to I.9B.005. |
| I.9B.007 | ex 9E002 | ‘ Technology ’ according to the General Technology Note for the ‘ production ’ of equipment specified in I.9A.001, I.9A.003 or I.9A.021 to I.9A.024. |
| I.9B.008 | 9E101 | ‘ Technology ’ according to the General Technology Note for the ‘ development ’ or ‘ production ’ of goods specified in I.9A.004 to I.9A.017. |
| I.9B.009 | ex 9E102 | ‘ Technology ’ according to the General Technology Note for the ‘ use ’ of space launch vehicles specified in I.9A.001, or goods specified in I.9A.002, I.9A.004 to I.9A.017, I.9A.020 to I.9A.024, I.9B.002 or I.9B.003.] |
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