(i) Valves, having both of the following:

a. A nominal size greater than 1.0 cm (3/8"), and

b. All surfaces that come in direct contact with the chemical(s) being produced, processed, or contained are made from the materials of construction in Technical Note 1 of this entry

(ii) Valves, not already identified in 3D001(6)(i), having all of the following:

a. A nominal size equal to or greater than 2.54 cm (1") and equal to or less than 10.16 cm (4")

b. Casings (valve bodies) or preformed casing liners.

c. A closure element designed to be interchangeable, and

d. All surfaces of the casing (valve body) or preformed case liner that come in direct contact with the chemical(s) being produced, processed, or contained are made from the materials of construction in Technical Note 1 of this entry

(iii) Components, as follows:

a. Casings (valve bodies) designed for valves in paragraphs 6.a.or 6.b., in which all surfaces that come in direct contact with the chemical(s) being produced, processed, or contained are made from the materials of construction in Technical Note 1 of this entry;

b. Preformed casing liners designed for valves in paragraphs 6.a.or 6.b.. in which all surfaces that come in direct contact with the chemical(s) being produced, processed, or contained are made from the materials of construction in Technical Note 1 of this entry.

Technical Note 1. Materials of construction for valves include any of the following:

a. nickel or alloys with more than 40% nickel by weight;

b. alloys with more than 25% nickel and 20% chromium by weight;

c. fluoropolymers (polymeric or elastomeric materials with more than 35% fluorine by weight);

d. glass or glass-lined (including vitrified or enamelled coating);

e. tantalum or tantalum alloys;

f. titanium or titanium alloys;

g. zirconium or zirconium alloys; h. niobium (columbium) or niobium alloys; or

i. ceramic materials as follows: 1.silicon carbide with a purity of 80% or more by weight;

2 .aluminum oxide (alumina) with a purity of 99.9% or more by weight:

3 .zirconium oxide (zirconia).

Technical Note 2. The 'nominal size' is defined as the smaller of the inlet and outlet port diameters.

(i) Valves, having both of the following:

a. A nominal size greater than DN 10 or NPS 3/8 or national equivalents, and

b. All surfaces that come in direct contact with the chemical(s) being produced, processed, or contained are made from the materials of construction in Technical Note 1 of this entry

(ii) Valves, not already identified in 3D001(6)(i), having all of the following:

a. A nominal size equal to or greater than DN 25 or NPS 1 and equal to or less than DN 100 or NPS 4 or national equivalents.

b. Casings (valve bodies) or preformed casing liners.

c. A closure element designed to be interchangeable, and

d. All surfaces of the casing (valve body) or preformed case liner that come in direct contact with the chemical(s) being produced, processed, or contained are made from the materials of construction in Technical Note 1 of this entry

(iii) Components, as follows:

a. Casings (valve bodies) designed for valves in paragraphs 6.a.or 6.b., in which all surfaces that come in direct contact with the chemical(s) being produced, processed, or contained are made from the materials of construction in Technical Note 1 of this entry;

b. Preformed casing liners designed for valves in paragraphs 6.a.or 6.b.. in which all surfaces that come in direct contact with the chemical(s) being produced, processed, or contained are made from the materials of construction in Technical Note 1 of this entry.

Technical Note 1. Materials of construction for valves include any of the following:

a. nickel or alloys with more than 40% nickel by weight;

b. alloys with more than 25% nickel and 20% chromium by weight;

c. fluoropolymers (polymeric or elastomeric materials with more than 35% fluorine by weight);

d. glass or glass-lined (including vitrified or enamelled coating):

e. tantalum or tantalum alloys;

f. titanium or titanium alloys;

g. zirconium or zirconium alloys;

h. niobium (columbium) or niobium alloys; or

i. ceramic materials as follows: 1.silicon carbide with a purity of 80% or more by weight;

2 .alum mum oxide (alumina) with a purity of 99.9% or more by weight;

3 .zirconium oxide (zirconia). Technical Note 2. The 'nominal size' is defined as the smaller of the inlet and outlet port diameters.

Technical Note 3. Me trie nominal sizes (DN) of valves are in accordance with 1SO6708:1995. National Pipe Sizes (NPS) are in accordance with ASME B36.10 or B36.19, or national equivalents.

(1) Fermenters capable of cultivation of microorganisms or of live cells for the production of viruses or toxins, without the propagation of aerosols, having a total internal volume of 20 litres or greater;

(2) Components designed for such fermenters, as follows:-

a. Cultivation chambers designed to be sterilized or disinfected in situ:

b. cultivation chamber holding devices: or

c. process control units capable of simultaneously monitoring and controlling two or more fermentation system parameters (e.g. temperature, pH, nutrients, agitation, dissolved oxygen, air flow, foam control).

Technical Note

Fermenters include bioreactors (including single-use (disposable) bioreactors), chemostats and continuous-flow systems.

(1) Fermenters capable of cultivation of microorganisms or of live cells for the production of viruses or toxins, without the propagation of aerosols, having a total internal volume of 20 litres or greater:

(2) Components designed for such fermenters, as follows:-

a. Cultivation chambers designed to be sterilized or disinfected in situ;

b. cultivation chamber holding devices; or

c. process control units capable of simultaneously monitoring and controlling two or more fermentation system parameters (e.g. temperature. pH. nutrients, agitation, dissolved oxygen, air flow, foam control).

Technical Note 1 Fermenters include bioreactors (including single-use (disposable) bioreactors), chemostats and continuous-flow systems.

Technical Note 2 Cultivation chamber holding devices include single-use cultivation chambers with rigid walls.

2D001 African Horse Sickness virus

2D002 African Swine Fever virus

2D003 Avian influenza virus Note This includes only those Avian injluet viruses of high pathogenicity as defined by , World Organization for Animal Health (Ol the European Onion (EO), or compeh national regulatory bodies.

2D004 Blue tongue virus

2D005 Camel pox virus

2D006 Chikungunya virus 2D007 Crimean-Congo hemorrhagic fever virus

2D008 Dengue virus

2D009 Eastern equine encephalitis virus

2D010 Ebolavirus: all members of the Ebolavii genus

2D011 Encephalomyocarditis virus (EMC)

2D012 Foot and Mouth Disease virus (all serotyp and subtypes)

2D013 Guanarito virus

2D014 Goatpox virus

2D015 Hantaan virus

2D016 Herpes virus simiae (monkey B virus)

2D017 Herpes ateles. Herpes saimiri

2D018 HIV- 1 & HlV-2 and other strains of SIV

2D019 Classical swine fever virus (Hog cholera viru

2D020 Human T-cell Leukemia virus

2D021 Junin virus

2D022 Japanese encephalitis virus

2D023 Kyasanur Forest Disease virus

2D024 Korean hemorrhagic fever virus

2D025 Lymphocytic choriomeningitis virus (LCM) 2D026 Lassa virus

2D027 Marburgvirus: all members of the Marburgvii genus

2D028 Murray valley encephalitis virus

2D029 Machupo virus

2D030 Mason-pfizer monkey virus

2D031 Monkey pox virus

2D032 Newcastle disease virus
2D033 Omsk hemorrhagic fever virus

2D034 Peste des petits ruminant virus

2D035 Teschen disease virus (Porcine entero virus type 1)

2D036 Powassan virus

2D037 Rabies virus and other members of the Lyssavirus genus

2D038 Respiratory syncitial virus

2D039 Rift Valley Fever virus

2D040 Rinderpest virus

2D041 Sabia virus

2D042 Sheeppox virus

2D043 Sin Nombre virus

2D044 Smallpox virus

2D045 St.Louisencephalitis virus

2D046 Swine vesicular disease virus

2D047 Tick-borne encephalitis virus (Far Eastern subtype)

2D048 (Reserved)

2D049 Variola virus

2D050 Venezuelan equine encephalitis virus

2D051 Vesicular stomatitis virus

2D052 Western equine encephalitis virus

2D053 Yellow fever virus

2D054 Andes virus

2D055 Chapare virus

2D056 Choclo virus

2D057 Dobrava-Belgrade virus

2D058 Suidherpesvirus 1 (Pseudorabies virus; Aujeszky's disease)

2D059 Hendra virus (Equine morbi Hi virus)

2D060 Laguna Negra virus

2D061 Louping ill virus

2D062 Lujo virus

2D063 Lumpy skin disease virus

2D064 (Reserved)

2D065 Nipah virus

2D066 Oropouche virus

2D067 (Reserved)

2D068 Rocio virus

2D069 Seoul virus

2D070 Severe acute respiratory syndrome-related coronavirus (SARS-related coronavirus)

2D071 Reconstructed 1918 influenza virus

2D001 African Horse Sickness virus

2D002 African Swine Fever virus

2D003 Avian influenza virus Note This includes only those Avi influenza viruses of high pathogenicity defined by the World Organization Animal Health (O1E), the European Oni (EO), or competent national regulate bodies.

2D004 Blue tongue virus

2D005 Camel pox virus

2D006 Chikungunya virus

2D007 Crimean-Congo hemorrhagic fever virus

2D008 Dengue virus

2D009 Eastern equine encephalitis virus 2D010 Ebolavirus: all members of the Ebolavii genus

2D011 Encephalomyocarditis virus (EMC) 2D012 Foot and Mouth Disease virus (all serotyp and subtypes)

2D013 Guanarito virus

2D014 Goatpoxvirus

2D015 Hantaan virus

2D016 Herpes virus simiae (monkey B virus)

2D017 Herpes ateles, Herpes saimiri 2D018 HIV- 1 & HIV-2 and other strains of SIV

2D019 Classical swine fever virus (Hog chok virus)

2D020 Human T-cell Leukemia virus 2D021 Junin virus

2D022 Japanese encephalitis virus

2D023 Kyasanur Forest Disease virus 2D024 Korean hemorrhagic fever virus 2D025 Lymphocytic choriomeningitis virus (LCM

2D026 Lassa virus

2D027 Marburgvirus: all members of the Marburgvirus genus

2D028 Murray valley encephalitis virus 2D029 Machupo virus

2D030 Mason-pfizer monkey virus

2D031 Middle East respiratory syndrome coronavirus (MERS-CoV)

2D032 Monkey pox virus

2D033 Newcastle disease virus

2D034 Omsk hemorrhagic fever virus

2D035 Peste des petits ruminant virus

2D036 Teschen disease virus (Porcine entero virus type 1)

2D037 Powassan virus

2D038 Rabies virus and other members of the Lyssavirus genus

2D039 Respiratory syncitial virus

2D040 Rift Valley Fever virus

2D041 Rinderpest virus

2D042 Sabia virus

2D043 Sheeppox virus

2D044 Sin Nombre virus

2D045 Smallpox virus

2D046 St.Louisencephalitis virus

2D047 Swine vesicular disease virus 2D048 Tick-borne encephalitis virus (Far Eastern subtype)

2D049 (Reserved)

2D050 Variola virus

2D051 Venezuelan equine encephalitis virus

2D052 Vesicular stomatitis virus

2D053 Western equine encephalitis virus 2D054 Yellow fever virus

2D055 Andes virus

2D056 Chapare virus

2D057 Choclo virus

2D058 Dobrava-Belgrade virus

2D059 Suidherpesvirus 1 (Pseudorabies virus: Aujeszky's disease)

2D060 Hendra virus (Equine morbillivirus)

2D061 Laguna Negra virus

2D062 Louping ill virus

2D063 Lujo virus

2D064 Lumpy skin disease virus

2D065 (Reserved)

2D066 Nipah virus

2D067 Oropouche virus

2D068 (Reserved)

2D069 Rocio virus

2D070 Seoul virus

2D071 Severe acute respiratory syndrome-related coronavirus (SARS-related coronavirus)

2D072 Reconstructed 1918 influenza virus

a. rocket motor cases, interior lining, insulation andnozzles;

b. rocket staging mechanisms, separation mechanisms andinter-stages:

c. Liquid, slurry and gel propellant (including oxidisers) control systems, and specially designedcomponents therefor, usable in missiles and rockets, designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz

Notes

1. The only servo valves, pumps and gas turbines specified in 5 A102.c are the following:

> Servo valves designed for flow rates equal to or greater than 24 litres per minute, atan absolute pressure equal to or greater than 7 MPa. that have an actuator response time of less than 100ms.

> Pumps, for liquid propellants, with shaft speeds equal to or greater than 8,000 rpmat the maximum operating mode or with discharge pressures equal to or greater than 7 Mpa

> Gas turbines, for liquid propellant turbopumps, with shaft speeds equal to or greater than 8,000 rpm at the maximum operating mode.

2. Systems and components specified in this clause may be exported as part of a satellite-.

d. re-entry vehicles and equipmentincluding

1. Heat-shields and components thereof, fabricated of ceramic orablative materials; 2. Heat sinks and components thereof, fabricated of light weight, high heat capacity materials;

3. Electronic equipment specially designed for re-entry vehicles.

e. guidance systems and their components such as gyros and inertial referenceunits;

f. thrust-vector control subsystems including methods of achieving thrust vector control such as flexible nozzle, fluid or secondary gas injection, movable engine or nozzle, deflection of exhaust gas stream (jet vanes or probes) and use of thrust tabs;

g. hybrid rocket motors and components thereof;

h. safing, arming, fusing and firing mechanisms for weapons orwarhead.

i. software specially designed for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acousti csignatures.

j. Combustion chambers and nozzles for liquid propellant rocket engines or gel propellant rocket motors

a. rocket motor cases, interior lining, insulation andnozzles;

b. rocket staging mechanisms, separation mechanisms andinter-stages:

c. Liquid, slurry and gel propellant (including oxidisers) control systems, and specially designedcomponents therefor, usable in missiles and rockets, designed or modified to operate in vibration environments greater than 10 grms between 20 Hz and 2 kHz.

Notes

1. The only servo valves, pumps and gas turbines specified in 5A102.c are the following:

a. Servo valves designed for flow rates equal to or greater than 24 litres per minute, atan absolute pressure equal to or greater than 7 MPa, that have an actuator response time of less than 100ms.

b. Pumps, for liquid propellants, with shaft speeds equal to or greater than 8,000 rpmat the maximum operating mode or with discharge pressures equal to or greater than 7 Mpa

c. Gas turbines, for liquid propellant turbopumps, with shaft speeds equal to or greater than 8,000 rpm at the maximum operating mode.

2. Systems and components specified in this clause may be exported as part of a satellite',

d. re-entry vehicles and equipmentincluding

1. Heat-shields and components thereof, fabricated of ceramic orablative materials; 2. Heat sinks and components thereof, fabricated of light weight, high heat capacitymaterials;

3. Electronic equipment specially designed for re-entry vehicles.

e. guidance systems and their components such as gyros and inertial referenceunits;

f. thrust-vector control subsystems including methods of achieving thrust vector control such as flexible nozzle, fluid or secondary gas injection, movable engine or nozzle, deflection of exhaust gas stream (jet vanes or probes) and use of thrust tabs:

g.hybrid rocket motors and components thereof:

h.safing. arming, fusing and firing mechanisms for weapons orwarhead.

i. software specially designed for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acousticsignatures.

j. Combustion chambers and nozzles for liquid propellant rocket engines or gel propellant rocket motors

k. Turbojet and turbofan engines (including turbo compound engines).

l. "Ramjet Scramjet, pulse jet, combined cycle engines, including devices to regulate combustion, and specially designed components."

e. Light weightTurbojet / turbofan engines (including turbo compound engines).

e. Light weightTurbojet and turbofan engines (including turbo compound engines).

1. Facilities or plants for the production, recovery, extraction, concentration or handling oftritium; 2. Equipment for tritium facilities or plants, asfollows;

i. Hydrogen or helium refrigeration units capable of cooling to 23 K (-250 °C) or less, with heat removalcapacity greater than 150 W;

ii. Hydrogen isotope storage or hydrogen isotope purification systems using metal hydrides as the storage or purificationmedium.

a. for use in a nuclear reactor or any other nuclear activities in quantities exceeding 1 kilogram;

b. for use in non-nuclear activities in quantities exceeding 30 metric tons for any one recipient country within a period of one calendar year.

Note The item 0A302 does not cover graphite powder.

Note 1 The item 0A302 does not cover graphite powder.

Note 2 For the purpose of export control, the Government will determine whether or not the exports of graphite meeting the above specifications are for nuclear reactor use. Graphite having a purity level better than 5 ppm (parts per million) boron equivalent and with a density greater than 1.50 g/cm3 not for use in a nuclear reactor or any other nuclear activities is not covered by this paragraph.

Boron Equivalent (BE) may be determined experimentally or is calculated as the sum of BEz for impurities (excluding BEcarbon since carbon is rot considered an impurity) including boron, where: BEz ppm = CF x concentration of element Z (in ppm); B x Az);az x AB) divided by (oCF is the conversion factor: ( z are the thermal neutron capture cross sections (in bams) for naturally er B and ct occurring boron and element Z respectively; and AB and Az are the atomic masses ol naturally occurring boron and element Z respectively

a. Irradiated fuel element chopping machines designed for remote operation

b. Dissolvers capable of withstanding hot and highly corrosive liquid for dissolution of irradiated nuclear fuel and which can be remotely loaded and maintain

c. Solvent extractors and solvent extraction equipment resistant to the corrosive effect of nitric acid

d. Chemical holding or storage vessels resistant to the corrosive effect of nitric acid

e. Neutron measurement systems for integration and use with automated process control systems for the reprocessing of irradiated fuel elements.

f. Industrial equipment including assemblies and components as follows:

1. High density (lead glass or other) radiation shielding windows 2. Radiation hardened TV cameras, or lenses therefor

3. 'Robots' or 'end effectors' especially designed for handling high explosives: and control units therefor

4. Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells

a. Irradiated fuel element decladding equipment and chopping machines: Remotely operated equipment especially designed or prepared for use in a reprocessing plant as identified above and intended to expose or prepare the irradiated nuclear material in fuel assemblies, bundles or rods for processing.

b. Dissolvers: Dissolver vessels or dissolvers employing mechanical devices especially designed or prepared for use in a reprocessing plant as identified above, intended for dissolution of irradiated nuclear fuel and which are capable of withstanding hot, highly corrosive liquid, and which can be remotely loaded, operated, and maintained. C. Solvent extractors and solvent extraction equipment: Especially designed or prepared solvent extractors (such as packed or pulse columns, mixer settlers or centrifugal contactors) for use in a plant for the reprocessing of irradiated fuel. Solvent extractors must be resistant to the corrosive effect of nitric acid. Solvent extractors are normally fabricated to extremely high standards special welding and inspection and quality assurance and quality control techniques) out of low carbon stainless steels, titanium, zirconium, or other high quality materials.

d. Chemical holding or storage vessels: Especially designed or prepared holding or storage vessels for use in a plant for the reprocessing of irradiated fuel. The holding or storage vessels must be resistant to the corrosive effect of nitric acid. The holding or storage vessels are normally fabricated of materials such as low carbon stainless steels, titanium or zirconium, or other high quality materials. Holding or storage vessels may be designed for remote operation and maintenance and may have the following features for control of nuclear criticality:

1. Walls or internal structures with a boron equivalent of at least 2%; 2. A maximum diameter of 175 mm for cylindrical vessels; or

3. A maximum width of 75 mm for either a slab or annular vessel.

e. Neutron measurement systems for process control Neutron measurement systems especially designed or prepared for integration and use with automated process control systems in a plant for the reprocessing of irradiated fuel elements.

f. (Deleted)

a. for use in a nuclear reactor in quantities exceeding 5 kilograms of deuterium atoms in one consignment or 25 kilograms of deuterium atoms, for any one recipient country within a period of one calendar year:

b. for use in a non-nuclear activity in quantities exceeding 200 kilograms of deuterium atoms, for any one recipient country within a period of one calendar year.

a. Made from any of the follow ing: 1. An organic "matrix" and "fibrous or filamentary materials" specified by 8C110.c. 8C110.dor

2. Prepregs or preforms specified by 8C110.e;

b. Made from a metal or carbon "matrix", and any of the following: 1. Carbon "fibrous or filamentary materials" having all of the following:

a. A "specific modulus" exceeding 10.15 x 10(6) m; and

b. A "specific tensile strength" exceeding 17.7 x 104 m; or

2. Materials specified by 8C110.c. Note 1 8A102 does not apply to "composite " structures or laminates, made from epoxy resin impregnated carbon "fibrous or filamentary materials", for the repair of "civil aircraft" structures or laminates, having all of the following:

a. An area not exceeding 1 m2;

b. A length not exceeding 2.5 m; and

c. A width exceeding 15 mm.

Note 2 8A102 does not apply to semi-finished items, specially designed for purely civilian applications as follows:

a. Sporting goods;

b. Automotive industry;

c. Machine tool industry;

d. Medical applications.

Note 3 8A102.b. 1. does not apply to semi-finished items containing a maximum of two dimensions of interwoven filaments and specially designed for applications as follows: a. Metal heat-treatment furnaces for tempering metals; b. Silicon boule production equipment.

Note 4 8A102 does not apply to finished items specially designed for a specific application.

a. Made from any of the following:

1. An organic "matrix" and "fibrous or filamentary materials" specified by 8C110.c, 8C110.dor

2. Prepregs or preforms specified by 8C110.e;

b. Made from a metal or carbon "matrix", and any of the following: 1. Carbon "fibrous or filamentary materials" having all of the following:

a. A "specific modulus" exceeding 10.15 x 10(6) m; and

b. A "specific tensile strength" exceeding 17.7 x 104 m; or

2. Materials specified by 8C110.c. Note 1 8A102 does not apply to "composite " structures or laminates, made from epoxy resin impregnated carbon "fibrous or filamentary materials", for the repair of "civil aircraft" structures or laminates, having all of the following:

a. An area not exceeding 1 m2;

b. A length not exceeding 2.5 m; and

c. A width exceeding 15 mm.

Note 2 8A102 does not apply to semi-finished items, specially designed for purely civilian applications as follows:

a. Sporting goods;

b. Automotive industry;

c. Machine tool industry;

d. Medical applications.

Note 3 8A102. b. 1. does not apply to semi-finished items containing a maximum of two dimensions of interwoven filaments and specially designed for applications as follows: a. Metal heat-treatment furnaces for tempering metals; b. Silicon boule production equipment.

Note 4 8A102 does not apply to finished items specially designed for a specific application.

Note 5 8A102.b.l. does not apply to mechanically chopped, milled, or cut carbon "fibrous or filamentary materials" 25.0 mm or less in length.

a. Soft body armour not manufactured to military standards or specifications, or to their equivalents, and specially designed components therefor:

b. Hard body armour plates providing ballistic protection equal to or less than level IIIA (NIJ 0101.06. July 2008)

N.B.1. For "fibrous or filamentary materials" used in the manufacture of body armour, see 8C110.

N.B.2. For body armour manufactured to military standards or specifications, see 6A013.d. Note 1 8A105 does not apply to body armour when accompanying its user for the user's own personal protection.

Note 2 8A105 does not apply to body armour designed to provide frontal protection only from both fragment and blast from non-military explosive devices. Note 3 8A105 does not apply to body armour designed to provide protection only from knife, spike, needle or blunt trauma.

N.B, 1. For "fibrous or filamentary materials" used in the manufacture of body armour, see 8C110.

N.B.2. For body armour manufactured to military standards or specifications, see 6A013.d. Note 1 8A105 does not apply to body armour when accompanying its user for the user's own personal protection.

Note 2 8A105 does not apply to body armour designed to provide frontal protection only from both fragment and blast from non-military explosive devices. Note 3 8A105 does not apply to body armour designed to provide protection only from knife, spike, needle or blunt trauma.

a. Remotely operated vehicles;

b. 'Disruptors';

Technical Note

'Disruptors' - Devices specially designed for the purpose of preventing the operation of an explosive device by projecting a liquid, solid or frangible projectile.

N.B. For equipment specially designed for military use for the disposal of improvised explosive devices, see also 6A004. Note 8A106 does not apply to equipment when accompanying its operator.

a. Remotely operated vehicles;

b. 'Disruptors';

Technical Note

For the purpose of 8A106. b., 'disruptors' are devices specially designed for the purpose ofpreventing the operation of an explosive device by projecting a liquid, solid or frangible projectile. N. B. For equipment specially designed for military use for the disposal of IE Ds. see also 6A004. Note 8A106 does not apply to equipment when accompanying its operator.

a. Materials for absorbing frequencies exceeding 2 x 108 Hz but less than 3x1012 Hz;

Note 1: 8C101. a does not apply to:

a. Hair type absorbers, constructed of natural or synthetic fibres, with non-magnetic loading to provide absorption:

b. Absorbers having no magnetic loss and whose incident surface is non-planar in shape, including pyramids, cones, wedges and convoluted surfaces;

c. Planar absorbers, having all of the following:

1. Made from any of the following: a. Plastic foam materials (flexible or non-fiexible) with carbon-loading, or organic materials, including binders, providing more than 5% echo compared with metal over a bandwidth exceeding ±15% of the centre frequency of the incident energy, and not capable of withstanding temperatures exceeding 450 K (177° C); or

b. Ceramic materials providing more than 20%> echo compared with metal over a bandwidth exceeding ±15% of the centre frequency of the incident energy, and not capable of withstanding temperatures exceeding 800 K (527°C);

2. Tensile strength less than 7x10(6) N/m(2) ; and

3. Compressive strength less than 14x10(6) N/m(2) ;

d. Planar absorbers made of sintered ferrite, having all of the following:

1. A specific gravity exceeding 4.4: and

2. A maximum operating temperature of 548 K (2 75 °C) or less;

a. Materials for absorbing frequencies exceeding 2 x 108 Hz but less than 3 x 1012 Hz;

Note 1: 8C101.a does not apply to:

a. Hair type absorbers, constructed of natural or synthetic fibres, with non-magnetic loading to provide absorption;

b. Absorbers having no magnetic loss and whose incident surface is non-planar in shape, including pyramids, cones, wedges and convoluted surfaces;

c. Planar absorbers, having all of the following:

1. Made from any of the following: a. Plastic foam materials (flexible or non-fiexible) with carbon-loading, or organic materials, including binders, providing more than 5% echo compared with metal over a bandwidth exceeding ±15%> of the centre frequency of the incident energy, and not capable of withstanding temperatures exceeding 450 K (177° C); or b. Ceramic materials providing more than 20%> echo compared with metal over a bandwidth exceeding ±15%> of the centre frequency of the incident energy, and not capable of withstanding temperatures exceeding 800 K (527°C);

2. Tensile strength less than 7 x 10(6) N/m(2) ; and

3. Compressive strength less than 14x10(6) N/m(2) ;

d. Planar absorbers made of sintered ferrite, having all of the following:

1. A specific gravity exceeding 4.4; and

2. A maximum operating temperature of 548 K (275°C) or less;

e. Planar absorbers having no magnetic loss and fabricated from 'open-cell foam' plastic material with a density of 0.15 grams/cm3 or less.

Technical Note 'Open-cell foams' are flexible and porous materials, having an inner structure open to the atmosphere. 'Opencell foams' are also known as reticulated foams.

Note 2: Nothing in Note 1 releases magnetic materials to provide absorption when contained in paint.

(See Commodity Identification Note I of SCOMET list)

Note 8C102 does not apply to metal alloys, metal alloy powder andalloyed materials, specially formulated for coating purposes. Technical Noles

1.The metal alloys in 8C102 are those containing a higher percentage by weight of the stated metal than of any other element.

2 .'Stress-rupture life'should be measured in accordance with ASTMstandard E-139.

3 . 'Low cycle fatigue life' should be measured in accordance with ASTM Standard E-606 'Recommended Practice for Constant-Amplitude Low-Cycle Fatigue Testing' or national equivalents. Testing should be axial with an average stress ratio equal to 1 and a stress-concentration factor (Kt) equal to 1. The average stress ratio is defined as maximum stress minus minimum stress divided by maximum stress.

(See Commodity Identification Note 1 of SCOMET list) Note 8C102 does not apply to metal alloys, metal alloy powder andalloyed materials, specially formulated for coating purposes. Technical Notes

1. The metal alloys in 8C102 are those containing a higher percentage by weight of the stated metal than of any other element.

2. 'Stress-rupture life' should be measured in accordance with ASTM standard E-139.

3. 'Low cycle fatigue life' should be measured in accordance with ASTM Standard E-606 'Recommended Practice for Constant-Amplitude Low-Cycle Fatigue Testing' or national equivalents. Testing should be axial with an average stress ratio equal to 1 and a stressconcentration factor (Kt) equal to 1. The average stress ratio is defined as maximum stress minus minimum stress divided by maximum stress.

Fluids and lubricating materials, as follows:

a. (Reserved)

b. Lubricating materials containing, as their principal ingredients, any of the following:

1. Phenylene or alkylphenylene ethers or thio-ethers, or their mixtures, containing more than two ether or thio-ether functions or mixtures thereof; or

2. Fluorinated silicone fluids with a kinematic viscosity of less than 5,000 mm2/s (5,000 centistokes) measured at 298 K (25°C);

c. Damping or flotation fluids having all of the following;

1. Purity exceeding 99.8%;

2. Containing less than 25 particles of 200 pm or larger in size per 100 ml: and

3. Made from at least 85% of any of the following:

a. Dibromotetrafluoroethane (CAS 25497-30-7, 124-73-2, 27336-23-8);

b. Polychlorotri fluoroethylene (oily and waxy modifications only); or

c. Polybromotri fluoroethylene;

d. Fluorocarbon fluids designed for electronic cooling and having all of the following:

1. Containing 85% by weight or more of any of the following, or mixtures thereof:

a. Monomeric forms of perfluoropolyalkylethertriazines or perfluoroaliphatic-ethers;

b. Perfluoroalkylamines;

c. Perfluorocycloalkanes; or

d. Perfluoroalkanes;

2. Density at 298 K (25°C) of 1.5 g/ml or more;

3. In a liquid state at 273 K (0°C); and

4. Containing 60% or more by weight of fluorine.

Note 8C106.d. does not apply to materials specified and packaged as medical products.

Fluids and lubricating materials, as follows:

a. (Reserved)

b. Lubricating materials containing, as their principal ingredients, any of the following:

1. Phenylene or alkylphenylene ethers or thio-ethers, or their mixtures, containing more than two ether or thioether functions or mixtures thereof; or

2. Fluorinated silicone fluids with a kinematic viscosity of less than 5.000 mm2/s (5,000 centistokes) measured at 298 K (25°C);

c. Damping or flotation fluids having all of the following:

1. Purity exceeding 99.8%;

2. Containing less than 25 particles of 200 pm or larger in size per 100 ml; and

3. Made from at least 85% of any of the following:

a. Dibromotetrafluoroethane (CAS 25497-30-7, 124-73- 2, 27336-23-8);

b. Polychlorotrifluoroethylene (oily and waxy modifications only); or

c. Polybromotrifluoroethylene; d. Fluorocarbon fluids designed for electronic cooling and having all of the following:

1. Containing 85% by weight or more of any of the following, or mixtures thereof:

a. Monomeric forms of perfluoropolyalkylethertriazines or perfluoroaliphatic-ethers;

b. Perfluoroalkylamines;

c. Perfluorocycloalkanes: or

d. Perfluoroalkanes;

2. Density at 298 K (25°C) of 1.5 g/ml or more;

3. In a liquid state at 273 K (0°C); and

4. Containing 60% or more by weight of fluorine.

Note 8C106.d. does not apply to materials specified and packaged as medical products.

1. "Specific modulus" exceeding 12.7 x 10(6) m; and

2. "Specific tensile strength" exceeding 23.5 x 10(4) m;

Note 8C110. a does not apply to polyethylene.

b. Carbon "fibrous or filamentary materials", having all of the following:

1. "Specific modulus" exceeding 14.65 x 10(6) m; and

2. "Specific tensile strength" exceeding 26.82 x 10(4) m;

Note 8C110. b does not apply to: a. "Fibrous or filamentary materials", for the repair of "civil aircraft" structures or laminates, having all of the following:

1. An area not exceeding 1m(2):

2. A length not exceeding 2.5 m: and

3. A width exceeding 15 mm.

b. Mechanically chopped, milled or cut carbon "fibrous or filamentary materials" 25.0 mm or less in length

c. Inorganic "fibrous or filamentary materials", having all of the following:

1. "Specific modulus" exceeding 2.54 x 10(6) m; and

2. Melting, softening, decomposition or sublimation point exceeding 1.922 K (1.649°C) in an inert environment:

Note 8C110.c does not apply to:

a. Discontinuous, multiphase, polycrystalline alumina fibres in chopped fibre or random mat form, containing 3% by weight or more silica, with a "specific modulus" of less than 10 x 106 m;

b. Molybdenum and molybdenum alloy fibres;

c. Boron fibres;

d. Discontinuous ceramic fibres with a melting, softening, decomposition or sublimation point lower than 2,043 K (1,770°C) in an inert environment.

1. "Specific modulus" exceeding 12.7 x 10(6)m: and

2. "Specific tensile strength" exceeding 23.5 x 10(4) m;

Note 8C110. a does not apply to polyethylene.

b. Carbon "fibrous or filamentary materials", having all of the following:

1. "Specific modulus" exceeding 14.65 x 10(6) m; and

2. "Specific tensile strength" exceeding 26.82 x 10(4) m;

Note 8C110. b does not apply to:

a. "Fibrous or filamentary materials", for the repair of "civil aircraft" structures or laminates, having all of the following:

1. An area not exceeding 1m(2);

2. A length not exceeding 2.5 m; and

3. A width exceeding 15 mm.

b. Mechanically chopped, milled or cut carbon "fibrous or filamentary materials" 25.0 mm or less in length.

c. Inorganic "fibrous or filamentary materials", having all of the following:

1. Having any of the following:

a. Composed of 50% or more by weight silicon dioxide and having a "specific modulus" exceeding 2.54 x 106 m; or

b. Not specified in 1.C. 10.c. 1 .a. and having a "specific modulus" exceeding 5.6 x 106 m; and

2. Melting, softening, decomposition or sublimation point exceeding 1,922 K (1.649°C) in an inert environment

Note 8C110.C does not apply to: a. Discontinuous, multiphase, polycrystalline alumina fibres in chopped fibre or random mat form, containing 3% by weight or more silica, with a "specific modulus" of less than 10x10(6) m;

b. Molybdenum and molybdenum alloy fibres;

c. Boron fibres;

d. Discontinuous ceramic fibres with a melting, softening, decomposition or sublimation point lower than 2,043 K (1,770°C) in an inert environment.

1. Anti-friction bearings and bearing systems, as follows, and components therefor:

Note 8A201 does not apply to balls with tolerances specified by the manufacturer in accordance with ISO 3290:2001 as grade G5 (or national equivalents) or worse.

a. Ball bearings and solid roller bearings, having all tolerances specified by the manufacturer in accordance with ISO 492 Tolerance Class 4 . or better, and having both 'rings' and 'rolling elements' (ISO 5593). made from monel or beryllium;

Note 8A201.a does not apply to tapered roller bearings.

Technical Notes

1. 'Ring' - annular part of a radial rolling bearing incorporating one or more raceways (ISO 5593:1997).

2. 'Rolling element'- ball or roller which rolls between raceways (ISO 5593:1997).

b. (Reserved)

c. Active magnetic bearing systems using any of the following: 1. Materials with flux densities of 2.0 T or greater and yield strengths greater than 414 Mpa:

2. All-electromagnetic 3D homopolar bias designs for actuators; or

3. High temperature (450 K (177°C) and above) position sensors.

a. Ball bearings and solid roller bearings, having all tolerances specified by the manufacturer in accordance with ISO 492 Tolerance Class 4 or Class 2 (or national equivalents), or better, and having both 'rings' and 'rolling elements', made from monel or beryllium:

Note: 8A201.a does not apply to tapered roller bearings.

Technical Notes

1. 'Ring' - annular part of a radial rolling bearing incorporating one or more raceways (ISO 5593:1997).

2. 'Rolling element'- ball or roller which rolls between raceways (ISO 5593:1997).

b. (Reserved)

c. Active magnetic bearing systems using any of the following, and specially designed components therefor:

1. Materials with flux densities of 2.0 T or greater and yield strengths greater than 414 Mpa:

2. All-electromagnetic 3D homopolar bias designs for actuators; or

3. High temperature(450 K (177°C) and above) position sensors.

2. All-electromagnetic 3D homopolar bias designs for actuators; or 3. High temperature (450 K (177°C) and above) position sensors.

1. Materials with flux densities of 2.0 T or greater and yield strengths greater than 414 Mpa;

2. All-electromagnetic 3D homopolar bias designs for actuators; or 3. High temperature(450 K (177°C) and above) position sensors.

Note 2 8B201 does not apply to special purpose machine tools limited to the manufacture of any of the following:

a. Crank shafts or cam shafts;

b. Tools or cutters;

c. Extruder worms;

d. Engraved or facetted jewellery parts; or

e. Dental pros theses;

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 8B201.a, b. or c.

Note 1 8B201 does not apply to special purpose machine tools limited to the manufacture of gears. For such machines, see 8B203.

Note 2 8B201 does not apply to special purpose machine tools limited to the manufacture of any of the following:

a. Crank shafts or cam shafts;

b. Tools or cutters;

c. Extruder worms;

d. Engraved or facetted jewellery parts; or

e. Dental pros theses;

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 8B201.a, b. or c.

Note 4 A machine tool having an additive manufacturing capability in addition to a turning, milling or grinding capability must be evaluated against each applicable entry 8B201.a., b. or c.

Note 8B301 .h. does not apply to multi-layer masks with a phase shift layer designed for the fabrication of memory devices not specified by 8A301.

Note 8B301 .h. does not apply to multi-layer masks with a phase shift layer designed for the fabrication of memory devices not specified bv 8A301. N.B. For masks and reticles, specially designed for optical sensors, see 8B602.

Technical Note 'Physics-based' in 8D303 means using computations to determine a sequence of physical cause and effect events based on physical properties (e.g., temperature, pressure, diffusion constants and semiconductor materials properties).

Note Libraries, design attributes or associated data for the design of semiconductor devices or integrated circuits are considered as "technology".

Technical Note 'Computational lithography' is the use of computer modelling to predict, correct, optimise and verify imaging oerformance of the lithography process over a range of patterns, processes, and system conditions.

a. A 'vector processor unit' designed to perform more than two calculations on floating-point vectors (one-dimensional arrays of 32-bit or larger numbers) simultaneously:

Technical Note

A 'vector processor unit' is a processor element with built-in instructions that perform multiple calculations on floating-point vectors (one-dimensiona! arrays of 32-bit or larger numbers) simultaneously, having at least one vector arithmetic logic unit and vector registers of at least 32 elements each.

b. Designed to perform more than four 64-bit or larger floating-point operation results per cycle: or

c. Designed to perform more than eight 16-bit fixed-point multiply-accumulate results per cycle (e.g., digital manipulation of analogue information that has been previously converted into digital form, also known as digital "signal processing").

Note 1 8E302 does not apply to "technology'"for multimedia extensions.

Note 2 8E302 does not apply to "technology"for micro-processor cores, having all of the following:

a Using "technology" at or above 0.130 pm: and

b. Incorporating multi-layer structures with five or fewer metal layers.

Note 3 8E302 includes "technology"for the "development" or "production" of digital signal processors and digital array processors.

a. A 'vector processor unit' designed to perform more than two calculations on 'floatingpoint' vectors (one-dimensional arrays of 32-bit or larger numbers) simultaneously;

Technical Note

A 'vector processor unit' is a processor element with built-in instructions that perform multiple calculations on 'floatingpoint' vectors (one-dimensional arrays of 32-bit or larger numbers) simultaneously, having at least one vector arithmetic logic unit and vector registers of at least 32 elements each.

b. Designed to perform more than four 64-bit or larger 'floating-point' operation results per cycle; or

c. Designed to perform more than eight 16-bit 'fixed-point' multiply-accumulate results per cycle (e.g., digital manipulation of analogue information that has been previously converted into digital form, also known as digital "signal processing").

Note 1 8E302 does not apply to "technology"for multimedia extensions.

Note 2 8E302 does not apply to "technology"for micro-processor cores, having all of the following:

a Using "technology" at or above 0.130 pm: and

b. Incorporating multi-layer structures with five or fewer metal layers.

Note 3 8E302 includes "technology"for the "development"or "production"of digital signal processors and digital array processors.

Technical Notes

1. For the purpose of 8E302.a. and 8E302.b., 'floating-point' is defined by IEEE-754.

2. For the purpose of 8E302.C.,fixed-point' refers to a fixed-width real number with both an integer component and a fractional component, and which does not include integer-only formats.

Technical Note

For the purpose of 8E304. 'SFQR' is the range of maximum deviation and minimum deviation from front reference plane, calculated by least square method with all front surface data including site boundary within a site.

a. "Technology" according to the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified by 8A4 or 8D4.

b. "Technology" according to the General Technology Note, other than that specified by 8E401 .a., for the "development" or "production" of equipment as follows:

1. "Digital computers" having an 'Adjusted Peak Performance' ('APP') exceeding 8.0 Weighted TeraFLOPS (WT);

2. "Electronic assemblies" specially designed or modified for enhancing performance by aggregation of processors so that the 'APP' of the aggregation exceeds the limit in 8E401.b.1

c. "Technology" for the "development" of "intrusion software".

Note 1: 8E401.a and 8E401.C do not apply to 'vulnerability disclosure' or 'cyber incident response'.

Note 2 Note I does not diminish national authorities' rights to ascertain compliance with 8E401.a and 8E401 .c

Technical Notes

1. 'Vulnerability disclosure' means the process of identifying, reporting, or communicating a vulnerability to. or analysing a vulnerability with, individuals or organizations responsible for conducting or coordinating remediation for the purpose of resolving the vulnerability.

2. 'Cyber incident response' means the process of exchanging necessary information on a cyber security incident with individuals or organizations responsible for conducting or coordinating remediation to address the cyber security incident.

a. "Technology" according to the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified by 8A4 or 8D4.

b. "Technology" according to the General Technology Note, other than that specified by 8E401.a., for the "development" or "production" of equipment as follows:

1 . "Digital computers" having an 'Adjusted Peak Performance' ('APP') exceeding 8.0 Weighted TeraFLOPS (WT):

2 ."Electronic assemblies" specially designed or modified for enhancing performance by aggregation of processors so that the 'APP' of the aggregation exceeds the limit in 8E40Lb.L

c. "Technology" for the "development" of "intrusion software".

Note 1: 8E401.a and 8E401.C do not apply to "vulnerability disclosure" or "cyber incident response ".

Note 2 Note 1 does not diminish national authorities' rights to ascertain compliance with 8E401.a and 8E401.C.

Technical Notes- Deleted

2. Equipment using techniques designed to enable radio communications in the same frequency channels on which co-located equipment specified by8A501.h.1 is transmitting.

N.B. See also Category 6.

2. Equipment using techniques designed to enable radio communications in the same frequency channels on which co-located equipment specified by 8A501.h.l is transmitting.

N.B. See also Category 6.

a. Analysis at the application layer (e.g, Layer 7 of Open Systems Interconnection (OSI) model (ISO/IEC 7498-1));

b. Extraction of selected metadata and application content (e.g, voice, video, messages, attachments); and

c. Indexing of extracted data; and 2. Being specially designed to carry out all of the following:

a. Execution of searches on the basis of 'hard selectors'; and

b. Mapping of the relational network of an individual or of a group of people.

Note 8A501J does not apply to systems or equipment, specially designed for any of the following: a. Marketing purpose:

b. Network Quality of Service (QoS); or

c. Quality of Experience (QoE).

Technical Note 'Hard selectors': data or set of data, related to an individual (e.g, family name, given name, e-mail, street address, phone number or group affiliations).

a. Analysis at the application layer (e.g. Layer 7 of Open Systems Interconnection (OSI) model (ISO/IEC 7498-1));

b. Extraction of selected metadata and application content (e.g, voice, video, messages, attachments); and

c. Indexing of extracted data; and 2.Being specially designed to carry out all of the following:

a. Execution of searches on the basis of "hard selectors"; and

b. Mapping of the relational network of an individual or of a group of people.

Note 8A501J does not apply to systems or equipment, specially designed for any of the following: Marketing purpose;

Network Quality of Service (QoS); or

Quality of Experience (QoE). Technical Note - Deleted

1. Execution of searches on the basis of "hard selectors" of either the content of communication or metadata acquired from a communications service provider using a 'handover interface'; and Technical Notes

1. For the purposes of 5.D.l.e., a 'handover interface' is a physical and logical interface, designed for use by an authorised law enforcement authority.

across which targeted interception measures are requested from a communications service provider and the results of interception are delivered from a communications service provider to the requesting authority. The 'handover interface' is implemented within systems or equipment (e.g., mediation devices) that receive and validate the interception request, and deliver to the requesting authority only the results of interception that fulfil the validated request.

2. 'Handover interfaces' may be specified by international standards (including but not limited to ETS1 TS 101 331, ETS1 TS101 671, 3GPP TS 33.108) or national equivalents. 2. Mapping of the relational network or tracking the movement of targeted individuals based on the results of searches on content of communication or metadata or searches as described in 5.D.1.e.1.

Note 8D501.e does not apply to "software" specially designed or modified for any of the following:

a. Billing purposes;

b. Network Quality of Service (QoS);

c. Quality of Experience (QoE);

d. Mediation devices; or

e. Mobile payment or banking use.

a. "Technology" according to the General Technology Note for the "development", "production" or "use" (excluding operation) of equipment functions or features specified by 8A501 or "software" specified by 8D501 .a:

b. Specific "technology" as follows: 1. "Required" "technology" for the "development" or "production" of telecommunications equipment specially designed to be used on board satellites;

2. "Technology" for the "development" or "use" of "laser" communication techniques with the capability of automatically acquiring and tracking signals and maintaining communications through exoatmosphere or subsurface (water) media;

a. "Technology" according to the General Technology Note for the "development", "production" or "use" (excluding operation) of equipment, functions or features specified by 8A501 or "software" specified by 8D501.a. or 8D501.e.;

b.Specific "technology" as follows: 1 ."Required" "technology" for the "development" or "production" of telecommunications equipment specially designed to be used on board satellites;

2 ."Technology" for the "development" or "use" of "laser" communication techniques with the capability of automatically acquiring and tracking signals and maintaining communications through exoatmosphere or sub-surface (water) media;

N.B. For "satellite navigation system " receiving equipment containing or employing decryption see 8A705., and for related decryption "software" and "technology" see 8D705.. And 8E701.

a. Designed or modified to use 'cryptography for data confidentiality' having a 'described security algorithm', where that cryptographic capability is usable, has been activated, or can be activated by means of "cryptographic activation" not employing a secure mechanism, as follows:

Remaining below entries under this sub-categories shall remain unchanged

N.B. For "satellite navigation system" receiving equipment containing or employing decryption see 8A705., and for related decryption "software" and "technology" see 8D705., and8E701.

a. Designed or modified to use 'cryptography for data confidentiality' having a 'described security algorithm', where that cryptographic capability is usable, has been activated, or can be activated by any means other than secure "cryptographic activation", as follows:

Remaining below entries under this sub-categories shall remain unchanged

1. Implement only published or commercial cryptographic standardstand

2. The cryptographic capability is limited to a nominal operating rangenot exceeding 30 metres according to the manufacturer specifications, or not exceeding 100 metres according to the manufacturer's specifications for equipment that cannot interconnectwith more than seven devices',

Routers, switches or relays, where the "information security" functionality is limited tothe tasks of "Operations, Administration or Maintenance" ("OAM") implementing onlypublished or commercial cryptographic standards:

Routers, switches, gateways or relays, where the "information security" functionality is limited to the tasks of "Operations. Administration or Maintenance" ("OAM") implementing only published or commercial cryptographic standards

Items, not specified by 8A405 or 8A504.a.. designed to perform all of the following:

1. 'Extract raw data' from a computing or communications device; and

2. Circumvent "authentication" or authorisation controls of the device, in order to perform the function described in 8A504.b.l. Technical Note

'Extract raw data' from a computing or communications device means to retrieve binary data from a storage medium, e.g. RAM. flash or hard disk, of the device without interpretation by the device's operating system or file system. Note 1 8A504. b. does not apply to systems or equipment specially designed for the "development" or "production" of a computing or communications device.

Note 2 8A504.b. does not include: a. Debuggers, hypervisors;

b. Items limited to logical data extraction:

c. Data extraction items using chip-off or JTAG; or

d. Items specially designed and limited to jailbreaking or rooting.

a. "Software" specially designed or modified for the "development", "production" or "use" of any of the following:

1. Equipment specified by 8A502 or "software" specified by 8D502.C.1;

2. Equipment specified by 8A503 or "software" specified by 8D502.C.2; or

3. Equipment specified by 8A504 or "software" specified by 8D502.C.3;

b. "Software" having the characteristics of a 'cryptographic activation token' specified by 8D502.b.

c. "Software" having the characteristics of. or performing or simulating the functions of. any of the following:

I. Equipment specified by 8A502.a.. 8A502.C.. 8A502.d. or 8A502.e.;

Note 8D502.C. 1. does not apply to "software" limited to the tasks of "OAM" implementing only published or commercial cryptographic standards.

2. Equipment specified by 8A503; or

3. Equipment specified by 8A504. d. (Reserved)

a. "Software" specially designed or modified for the "development", "production" or "use" of any of the following:

1. Equipment specified by 8A502 or "software" specified by 8D502.C. 1;

2. Equipment specified by 8A503 or "software" specified by 8D502.C.2; or

3. Equipment or "software", as follows:

a. Equipment specified by 8A504.a. or "software" specified by 8D502.c.3.a.;

b. Equipment specified by 8A504.b. or "software" specified by 8D502.c.3.b.;

b. "Software" having the characteristics of a 'cryptographic activation token' specified by 8D502.b.

c. "Software" having the characteristics of, or performing or simulating the functions of, any of the following:

1. Equipment specified by 8A502.a., 8A502.C., 8A502.d. or 8A502.e.;

Note 8D502.C.1. does not apply to "software" limited to the tasks of "OAM" implementing only published or commercial cryptographic standards.

2. Equipment specified by 8A503; or

3. Equipment, as follows:

a. Equipment specified by 8A504.a.;

b. Equipment specified by 8A504.b.

Note 8D502.c.3.b. does not apply to "intrusion software".

b. Equipment specified by 8A504.b.

Note 8D502.c3.b. does not apply to "intrusion software".

a. "Technology" according to the General Technology Note for the "development", "production" or "use" of equipment specified by 8A502. 8A503, 8A504 or 8B502, or of "software" specified by 8D502.a or 8D502.c;

b. "Technology" having the characteristics of a 'cryptographic activation token' specified by 8E502.b.;

Note 8E502.a. does not apply to "technology"for items specified by 8A304.b.,8D502.a.3.b. or 8D502.c.3.b.

"Space-qualified" components for optical systems, as follows:

1. Components lightweighted to less than 20% "equivalent density" compared with a solid blank of the same aperture and thickness:

2. Raw substrates, processed substrates having surface coatings (single-layer or multi-layer. metallic or dielectric, conducting, semiconducting or insulating) or having protective films;

3. Segments or assemblies of mirrors designed to be assembled in space into an optical system with a collecting aperture equivalent to or larger than a single optic 1 m in diameter;

4. Components manufactured from "composite" materials having a coefficient of linear thermal expansion equal to or less than 5 x 10-6 in any coordinate direction;

"Space-qualified" components for optical systems, a; follows:

1. Components lightweighted to less than 20% "equivalent density" compared with a solid blank of the same aperture and thickness;

2. Raw substrates, processed substrates having surface coatings (singlelayer or multi-layer, metallic or dielectric, conducting, semiconducting or insulating) or having protective films;

3. Segments or assemblies of mirrors designed to be assembled in space into an optical system with a collecting aperture equivalent to or larger than a single optic 1 m in diameter;

4. Components manufactured from "composite" materials having a coefficient of linear thermal expansion, in any coordinate direction, equal to or less than 5 x 10-6/K;

a. 'Single transverse mode' output and any of the following:

1. Average output power exceeding 1,000 W: or

2. Having all of the following: a. Average output power exceeding 500 W; and

b. Spectral bandwidth less than 40 GHz: or

a. 'Single transverse mode' output and any of the following:

1. Output power exceeding 1,000 W; or

2. Having all of the following: a. Output power exceeding 500 W: and

b. Spectral bandwidth less than 40 GHz; or

a. 'Single transverse mode' output and any of the following:

1. Average output power exceeding 1.000 W; or

2. Having all of the following:

a. Average output power exceeding 500 W; and b. Spectral bandwidth less than 40 GHz; or

b. 'Multiple transverse mode" output and any of the following:

1. 'Wall-plug efficiency' exceeding 18% and output power exceeding 1000 W;or

2. Output power exceeding 2 kW;

Note 1 8A605.a.6.b. does not apply to 'multiple transverse modeindustrial "lasers"with output power exceeding 2 kW and not exceeding 6 kW with a total mass greater than 1,200 kg. For the purpose of this note, total mass includes all components required to operate the "laser", e.g., "laser", nower supply, heal exchanger, but excludes external optics for beam conditioning or delivery'.

Note 2 8A605.a.6.b. does not apply to 'multiple transverse mode industrial "lasers" having any of the following:

a. (Reserved)

b. Output power exceeding 1 kW but not exceeding 1.6 kW and having a BPP exceeding 1.25 mm'mrad;

c. Output power exceeding 1.6 kW but not exceeding 2.5 kW and having a BPP exceeding 1.7 mm*mrad;

d. Output power exceeding 2.5 kW but not exceeding 3.3 kW and having a BPP exceeding 2.5 mm*mrad;

e. Output power exceeding 3.3 kW but not exceeding 6 kW and having a BPP exceeding 3.5 mnrmrad;

f. (Reserved)

g. (Reserved)

h. Output power exceeding 6 k W but not exceeding 8 kW and having a BPP exceeding 12 mwrnrad; or

i. Output power exceeding 8 k W but not exceeding 10 kW and having a BPP exceeding 24 mm*mrad;

Technical Note For the purpose of 6.A.5.a.6.b.. Note 2.a., 'brightness' is defined as the output power of the "laser" divided by the squared Beam Parameter Product (BPP), i.e., (output power)/BPP . Technical Note 'Wall-plug efficiency' is defined as the ratio of "laser" output power (or "average output power") to total electrical input power required to operate the "laser", including the power supply/conditioning and thermal conditioning/heat exchanger

a. 'Single transverse mode' output and any of the following:

1. Output power exceeding 1.000 W: or

2. Having all of the following: a. Output power exceeding 500 W; and

b. Spectral bandwidth less than 40 GHz: or

b. 'Multiple transverse mode' output and any of the following:

1. 'Wall-plug efficiency' exceeding 18% and output power exceeding 1000 W;or

2. Output power exceeding 2 kW; 8A605.a.6.b. does not apply to 'multiple transverse mode industrial "lasers"with output power exceeding 2 kW and not exceeding 6 kW with a total mass greater than 1,200 kg. For the purpose of this note, total mass includes all components required to operate the "laser", e.g., "laser", power supply, heat exchanger, but excludes external optics for beam conditioning or delivery. 8A605.a.6.b. does not apply to 'multiple transverse mode', industrial "lasers" having any of the following:

(Reserved)

Output power exceeding 1 kW but not exceeding 1.6 kW and having a BPP exceeding 1.25 mm*mrad;

Output power exceeding 1.6 kW but not exceeding 2.5 kW and having a BPP exceeding 1.7 mm*mrad;

Output power exceeding 2.5 kW but not exceeding 3.3 kW and having a BPP exceeding 2.5 mm*mrad:

Output power exceeding 3.3 kW but not exceeding 6 kW and having a BPP exceeding 3.5 mnrmrad;

(Reserved)

(Reserved)

Output power exceeding 6 kW but not exceeding 8 kW and having a BPP exceeding 12 mm*mrad; or

Output power exceeding 8 kW but not exceeding 10 kW and having a BPP exceeding 24 mmvnrad; Technical Note -deleted

Technical Note 'Wall-plug efficiency' is defined as the ratio of "laser" output power (or "average output power") to total electrical input power required to operate the "laser", including the power supply/conditioning and thermal conditioning/heat exchanger

Note 8A608. i does not apply to:

a. Fishing ground surveillance radar;

b. Ground radar equipment specially designed for enroute air traffic control and having all of the following:

1. A maximum 'instrumented range ' of 500 km or less;

2. Configured so that radar target data can be transmitted only one way from the radar site to one or more civil A TC centres;

3. Contains no provisions for remote control of the radar scan rate from the enroute ATC centre: and

4. Permanently installed.

c. Weather balloon tracking radars. Technical Note For the purposes of 8A608.i., 'instrumented range' is the specified unambiguous display range of a radar.

Note 8A608. i does not apply to:

a. Fishing ground surveillance radar; b. Ground radar equipment specially designed for enroute air traffic control and having all of the following:

1 .A maximum 'instrumented range ' of 500 km or less;

2 . Configured so that radar target data can be transmitted only one way from the radar site to one or more civil ATC centres;

3 . Contains no provisions for remote control of the radar scan rate from the enroute ATC centre; and

4 .Permanently installed.

c. Weather balloon tracking radars. Technical Note For the purposes of 8A608.i., 'instrumented range' is the specified unambiguous display range of a radar.

Technical Note

In 8A911, 'combined cycle engines' are the engines that employ two or more cycles of the following types of engines: gas-turbine engine (turbojet, turboprop, turbofan and turbo shaft), ramjet, scramjet, pulse jet, pulse detonation engine, rocket motor (liquid/gel/solid-propellant and hybrid).

Technical Note

For the purposes of 8A911., 'combined cycle engines' combine two or more of the following types of engines:

- Gas turbine engine (turbojet, turboprop and turbofan);

- Ramjet or scramjet;

- Rocket motor or engine (liquid/gel/solid-propellant and hybrid).

"Unmanned Aerial Vehicles" ("UAVs"), unmanned "airships", related equipment and components, as follows:

a. "UAVs" or unmanned "airships", designed to have controlled flight out of the direct 'natural vision' of the 'operator' and having any of the following:

1. Having all of the following:

a. A maximum 'endurance' greater than or equal to 30 minutes but less than 1 hour; and

b. Designed to take-off and have stable controlled flight in wind gusts equal to or exceeding 46.3 km/h (25 knots); or

2. A maximum 'endurance' of 1 hour or greater;

Technical Notes

1. For the purposes of 8A912.a. 'operator' is a person who initiates or commands the "UA V" or unmanned "airship" flight.

2. For the purposes of 8A9l2.a, 'endurance' is to be calculated for ISA conditions (ISO 2533:1975) at sea level in zero wind.

3. For the purposes of

"Unmanned Aerial Vehicles" ("UAVs"), unmanned "airships", related equipment and components, as follows: N.B. For "UAVs" that are "sub-orbital craft", see 9.A.4.h.

a. "UAVs" or unmanned "airships", designed to have controlled flight out of the direct 'natural vision' of the 'operator' and having any of the following:

1. Having all of the following:

a. A maximum 'endurance' greater than or equal to 30 minutes but less than 1 hour; and

b. Designed to take-off and have stable controlled flight in wind gusts equal to or exceeding 46.3 km/h (25 knots); or

2. A maximum 'endurance' of 1 hour or greater;

Technical Notes

1. For the purposes of8A912.a, 'operator' is a person who initiates or commands the "UA V" or unmanned "airship"flight.

2. For the purposes of 8A912.a, 'endurance' is to be calculated for ISA conditions (ISO 2533:1975) at sea level in zero wind.

3. For the purposes of 8A912.a, 'natural vision' means unaided human sight, with or without corrective lenses.

6A001.a. Rifles and combination guns, handguns, machine.sub-machine and volley guns;

Note 6A001.a does not apply to the following:

a. Rifles and combination guns, manufactured earlier than 1938;

b. Reproductions of rifles and combination guns, the originals of which were manufactured earlier than 1890;

c. Handguns, volley guns and machine guns, manufactured earlier than 1890, and their reproductions; d. Rifles or handguns, specially designed to discharge an inert projectile by compressed air or CO2

Note 6A001.a does not apply to the following:

a. Rifles and combination guns, manufactured earlier than 1938;

b. Reproductions of rifles and combination guns, the originals of which were manufactured earlier than 1890;

c. Handguns, volley guns and machine guns, manufactured earlier than 1890, and their reproductions; d. Rifles or handguns, specially designed to discharge an inert projectile by compressed air or CO2-

e. Handguns specially designed for any of the following:

1. Slaughtering of domestic animals 2. Tranquilising of animals.

1. Specially designed for military use; and

2. Specially designed for weapons specified in 6A002.a;

6A002 d. Mountings and detachable cartridge magazines. specially designed for the weapons specified in 6A002.a.

1. Weapon sights and weapon sight mounts, specially designed for military use;

2. Signature reduction devices;
3. Mountings;

4. Detachable cartridge magazines; 6A002.d. (Reserved)

1. Vehicles having all of the following:

a. Manufactured or fitted with materials or components to provide ballistic protection equal to or better than level III (NIJ 0108.01. September 1985. or comparable national standard):

b. A transmission to provide drive to both front and rear wheels simultaneously, including those vehicles having additional wheels for load bearing purposes whether driven or not;

c. Gross Vehicle Weight Rating (GVWR) greater than 4.500 kg; and d. Designed or modified for off-road use;

e. Mine-Protected vehicle

2. Components having all of the following:

a. Specially designed for vehicles specified in 6A006.b.1.;

And

5. Providing ballistic protection equal to or better than level III (NIJ 0108.01, September 1985. or comparable national standard).

1. Vehicles having all of the following:

a. Manufactured or fitted with materials or components to provide ballistic protection equal to or better than level III (NIJ 0108.01, September 1985), or "equivalent standards";

b. A transmission to provide drive to both front and rear wheels simultaneously, including those for vehicles having additional wheels for load bearing purposes whether driven or not;

c. Gross Vehicle Weight Rating (GVWR) greater than 4.500 kg; and d. Designed or modified for off-road use;

e. Mine-Protected vehicle

2. Components having all of the following:

a. Specially designed for vehicles specified in 6A006.b.L: and

b. Providing ballistic protection equal to or better than level III (NU 0108.01, September 1985), or "equivalent standards".

1. Nuclear power generating equipment or propulsion equipment, specially designed for vessels specified in 6A009.a. and components therefor specially designed or modified' for military use.

Technical Note For the purpose of 6A009.h. 'modified' means any structural, electrical, mechanical, or other change that provides a non-military item with military capabilities equivalent to an item which is specially designed for military use.

Note 6A009.h.1. includes "nuclear reactors".

N.B See Commodity Identification Note 2 to SCOMET.

Technical Note For the purpose of 6A009.h., 'modified' means any structural, electrical, mechanical, or other change that provides a non-military item with military capabilities equivalent to an item which is specially designed for military use.

Note 6A009.h. includes "nuclear reactors".

Hard body armour plates providing ballistic protection equal to or greater than level III (NIJ 0101.06. July 2008).

a. Specially designed or modified 'production' equipment for the 'production' of products specified by Category 6, and specially designed components therefor:

b.Specially designed environmental test facilities and specially designed equipment therefor, for the certification, qualification or testing of products specified by Category 6.

a. "Software" specially designed or modified for any of the following:

1. "Development", "production", operation or maintenance of equipment specified by Category 6: 2. "Development" or "production" of materials specified by Category 6; or

3. "Development", "production", operation or maintenance of "software" specified by Category 6. b. Specific "software", other than that specified by 6A021 .a as follows:

1. "Software" specially designed for military use and specially designed for modelling, simulating or evaluating military weapon systems: 2. "Software" specially designed for military use and specially designed for modelling or simulating military operational scenarios;

3. "Software" for determining the effects of conventional, nuclear, chemical or biological weapons;

4. "Software" specially designed for military use and specially designed for Command, Communications, Control and Intelligence (C3I) or Command, Communications, Control, Computer and Intelligence (C4I) applications;

Note 2 6A021.b.5. does not apply to "vulnerability disclosure" or to "cyber incident response", limited to non-military defensive cybersecurity readiness or response.

N.B. See systems, equipment or components specified by Category 6 for general purpose "digital computers" with installed "software" specified by 6A021.C.

defined

Comparable national or international standards recognised by one or more Wassenaar Arrangement Participating States and applicable to the relevant entry.

Data or set of data, related to an individual (e.g., family name, given name, e-mail, street address, phone number or group affiliations).

The specified unambiguous display range of a radar.

a. Allows an arbitrary number of independent or interconnected 'data devices' to communicate directly with each other; and

b. Is confined to the communication between devices within the immediate vicinity of an individual person or device controller (e.g., single room, office, or automobile, and their nearby surrounding spaces).

Technical Note

'Data device' means equipment capable of transmitting or receiving sequences of digital information.

a. Allows an arbitrary number of independent or interconnected 'data devices' to communicate directly with each other: and

b. Is confined to the communication between devices within the immediate physical vicinity of an individual person or device controller (e.g., single room, office or automobile). Technical Notes

1. 'Data device' means equipment capable oj transmitting or receiving sequences of digital information.

2. The "local area network" extends beyona the geographical area of the "personal area network".

a. Operate above the stratosphere; b. Perform a non-orbital trajectory; and

c. Land back on Earth with the people or cargo intact.

"Circular Error Probable (CEP)" In a circular normal distribution, the radius of the circle containing 50% of the individual measurements being made, or the radius of the circle within which there is a 50% probability of being located.

"Circular Error Probable (CEP) or Circle of Equal Probability" In a circular normal distribution, the radius of the circle containing 50% of the individual measurements being made, or the radius of the circle within which there is a 50% probability of being located.