Textual Amendments
The entries do not always provide a complete description of the items and the related notes in Annex I. Only Annex I provides a complete description of the items. The terms appearing in straight double quotes are defined terms in the global definitions list of Annex I.
The mention of an item in this Annex does not affect the application of the General Software Note (GSN) in Annex I.
all items specified in Annex IV,
0C001 ‘ Natural uranium ’ or ‘ depleted uranium ’ or thorium in the form of metal, alloy, chemical compound or concentrate and any other material containing one or more of the foregoing,
0C002 ‘ Special fissile materials ’ other than those specified in Annex IV,
0D001 ‘ Software ’ specially designed or modified for the ‘ development ’ , ‘ production ’ or ‘ … ’ of goods specified in Category 0, in so far as it relates to 0C001 or to those items of 0C002 that are excluded from Annex IV,
0E001 ‘ Technology ’ in accordance with the Nuclear Technology Note for the ‘ development ’ , ‘ production ’ or ‘ … ’ of goods specified in Category 0, in so far as it relates to 0C001 or to those items of 0C002 that are excluded from Annex IV,
1A102 Resaturated pyrolized carbon-carbon components designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104,
1C351 Human and animal pathogens and ‘ toxins ’ ,
1C353 Genetic elements and genetically modified organisms,
1C354 Plant pathogens,
1C450.a.1. Amiton: O,O-Diethyl S-[2-(diethylamino)ethyl] phosphorothiolate (CAS 78-53-5) and corresponding alkylated or protonated salts,
1C450.a.2. PFIB: 1,1,3,3,3-Pentafluoro-2-(trifluoromethyl)-1-propene (CAS 382-21-8),
7E104 ‘ Technology ’ for the integration of flight control, guidance and propulsion data into a flight management system for optimisation of rocket system trajectory,
9A009.a. Hybrid rocket propulsion systems having total impulse capacity exceeding 1,1 MNs,
9A117 Staging mechanisms, separation mechanisms and interstages usable in ‘ missiles ’ .]