LegalizeCommission Implementing Regulation (EU) 2016/1375 of 29 July 2016 amending Council Regulation (EU) No 267/2012 concerning restrictive measures against Iran
This is the act as published. Later amendments are not folded into the text below: each one is a separate act in this repository and an entry in this law's history.
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 2A001 | Anti-friction bearings and bearing systems, as follows, and components therefor: N.B.: SEE ALSO 2A101. Note: 2A001 does not control balls with tolerances specified by the manufacturer in accordance with ISO 3290 as grade 5 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 national equivalents), or better, and having both rings and rolling elements (ISO 5593), made from monel or beryllium; Note: 2A001.a. does not control tapered roller bearings. b. Not used; 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. | M3A7 | Radial ball bearings having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all 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. |
| 2A101 | Radial ball bearings, other than those specified in 2A001, having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all the following characteristics: a. An inner ring bore diameter between 12 mm and 50 mm; b. An outer ring outside diameter between 25 mm and 100 mm; and c. A width between 10 mm and 20 mm. | M3A7 | Radial ball bearings having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all 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. |
| 2B004 | Hot “isostatic presses” having all of the following, and specially designed components and accessories therefor: N.B.: SEE ALSO 2B104 and 2B204. a. A controlled thermal environment within the closed cavity and a chamber cavity with an inside diameter of 406 mm or more; and b. Having any of the following: 1. A maximum working pressure exceeding 207 MPa; 2. A controlled thermal environment exceeding 1 773 K (1 500 °C); or 3. A facility for hydrocarbon impregnation and removal of resultant gaseous degradation products. Technical Note: 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. N.B.: For specially designed dies, moulds and tooling see 1B003, 9B009 and the Military Goods Controls. | M6B3 | Isostatic presses having all of the following characteristics: a) Maximum working pressure equal to or greater than 69 MPa; b) Designed to achieve and maintain a controlled thermal environment of 600 °C or greater; and c) Possessing a chamber cavity with an inside diameter of 254 mm or greater. |
| 2B009 | Spin-forming machines and flow-forming machines, which, according to the manufacturer's technical specification, can be equipped with “numerical control” units or a computer control and having all of the following: N.B.: SEE ALSO 2B109 AND 2B209. a. Three or more axes which can be coordinated simultaneously for “contouring control”; and b. A roller force more than 60 kN. Technical Note: For the purpose of 2B009, machines combining the function of spin-forming and flow-forming are regarded as flow-forming machines. | M3B3 | Flow-forming machines, and specially designed components therefor, which: a) According to the manufacturers technical specification can be equipped with numerical control units or a computer control, even when not equipped with such units at delivery; and b) Have more than two axes which can be co-ordinated simultaneously for contouring control. Note: This item does not include machines that are not usable in the “production” of propulsion components and equipment (e.g. motor cases) for systems specified in 1.A. Technical Note: Machines combining the function of spin-forming and flow-forming are, for the purpose of this item, regarded as flow-forming machines. |
| 2B104 | “Isostatic presses”, other than those specified in 2B004, having all of the following: N.B.: SEE ALSO 2B204. 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. | M6B3 | Isostatic presses having all of the following characteristics: a) Maximum working pressure equal to or greater than 69 MPa; b) Designed to achieve and maintain a controlled thermal environment of 600 °C or greater; and c) Possessing a chamber cavity with an inside diameter of 254 mm or greater. |
| 2B105 | Chemical vapour deposition (CVD) furnaces, other than those specified in 2B005.a., designed or modified for the densification of carbon-carbon composites. | M6B4 | Chemical vapour deposition furnaces designed or modified for the densification of carbon-carbon composites. |
| 2B109 | Flow-forming machines, other than those specified in 2B009, and specially designed components as follows: N.B.: SEE ALSO 2B209. 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 2B009 or 2B109.a. Note: 2B109 does not control machines that are not usable in the production of propulsion components and equipment (e.g. motor cases) for systems specified in 9A005, 9A007.a. or 9A105.a. Technical Note: Machines combining the function of spin-forming and flow-forming are for the purpose of 2B109 regarded as flow-forming machines. | M3B3 | Flow-forming machines, and specially designed components therefor, which: a) According to the manufacturers technical specification can be equipped with numerical control units or a computer control, even when not equipped with such units at delivery; and b) Have more than two axes which can be co-ordinated simultaneously for contouring control. Note: This item does not include machines that are not usable in the “production” of propulsion components and equipment (e.g. motor cases) for systems specified in 1.A. Technical Note: Machines combining the function of spin-forming and flow-forming are, for the purpose of this item, regarded as flow-forming machines. |
| 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 while 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 control bandwidth’ greater than 5 kHz designed for use with vibration test systems specified in 2B116.a.; Technical Note: In 2B116.b., ‘real-time control bandwidth’ means the maximum rate at which a controller can execute complete cycles of sampling, processing data and transmitting control signals. 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 2B116.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 2B116.a. Technical Note: In 2B116, ‘bare table’ means a flat table, or surface, with no fixture or fittings. | M15B1 | Vibration test equipment, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A. or 20.A., 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 while 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 control bandwidth’ greater than 5 kHz and designed for use with vibration test systems specified in 15.B.1.a.; Technical Note: ‘Real-time control bandwidth’ is defined as the maximum rate at which a controller can execute complete cycles of sampling, processing data and transmitting control signals. 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 15.B.1.a.; d) Test piece support structures and electronic units designed to combine multiple shaker units into a complete shaker system capable of providing an effective combined force equal to or greater than 50 kN, measured ‘bare table’, and usable in vibration test systems specified in 15.B.1.a. Technical Note: Vibration test systems incorporating a digital controller are those systems, the functions of which are, partly or entirely, automatically controlled by stored and digitally coded electrical signals. |
| 2B117 | Equipment and process controls, other than those specified in 2B004, 2B005.a., 2B104 or 2B105, designed or modified for densification and pyrolysis of structural composite rocket nozzles and reentry vehicle nose tips. | M6B5 | Equipment and process controls, other than those specified in 6.B.3. or 6.B.4., designed or modified for densification and pyrolysis of structural composite rocket nozzles and re-entry vehicle nose tips. |
| 2B119 | Balancing machines and related equipment, as follows: N.B.: SEE ALSO 2B219 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: 2B119.a. does not control balancing machines designed or modified for dental or other medical equipment. | M9B2a | Equipment as follows: 1. 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; |
| 2B119 | b. Indicator heads designed or modified for use with machines specified in 2B119.a. Technical Note: Indicator heads are sometimes known as balancing instrumentation. | M9B2b | Indicator heads (sometimes known as balancing instrumentation) designed or modified for use with machines specified in 9.B.2.a.; |
| 2B120 | Motion simulators or rate tables having all of the following characteristics: a. Two axes or more; b. Designed or modified to incorporate slip rings or integrated non-contact devices capable of transferring electrical power, signal information, or both; 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 less (better) than 5 arc second. Note 1: 2B120 does not control rotary tables designed or modified for machine tools or for medical equipment. For controls on machine tool rotary tables see 2B008. Note 2: Motion simulators or rate tables specified in 2B120 remain controlled whether or not slip rings or integrated non-contact devices are fitted at time of export. | M9B2c | Motion simulators/rate tables (equipment capable of simulating motion) having all of the following characteristics: 1. Two axes or more; 2. Designed or modified to incorporate sliprings or integrated non-contact devices capable of transferring electrical power, signal information, or both; and 3. Having any of the following characteristics: a. For any single axis having all of the following: 1. Capable of rates of 400 degrees/s or more, or 30 degrees/s or less; and 2. A rate resolution equal to or less than 6 degrees/s and an accuracy equal to or less than 0,6 degrees/s; b. Having a worst-case rate stability equal to or better (less) than plus or minus 0,05 % averaged over 10 degrees or more; or c. A positioning “accuracy” equal to or less (better) than 5 arc second. |
| 2B121 | Positioning tables (equipment capable of precise rotary positioning in any axes), other than those specified in 2B120, having all the following characteristics: a. Two axes or more; and b. A positioning “accuracy” equal to or less (better) than 5 arc second. Note: 2B121 does not control rotary tables designed or modified for machine tools or for medical equipment. For controls on machine tool rotary tables see 2B008 | M9B2d | Positioning tables (equipment capable of precise rotary positioning in any axes) having the following characteristics: 1. Two axes or more; and 2. A positioning “accuracy” equal to or less (better) than 5 arc second; |
| 2B122 | Centrifuges capable of imparting accelerations above 100 g and designed or modified to incorporate slip rings or integrated non-contact devices capable of transferring electrical power, signal information, or both. Note: Centrifuges specified in 2B122 remain controlled whether or not slip rings or integrated non-contact devices are fitted at time of export | M9B2e | Centrifuges capable of imparting accelerations above 100 g and designed or modified to incorporate sliprings or integrated non-contact devices capable of transferring electrical power, signal information, or both |
2D Software
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 2D001 | “Software”, other than that specified in 2D002, as follows: a. “Software” specially designed or modified for the “development” or “production” of equipment specified in 2A001 or 2B001 b. “Software” specially designed or modified for the “use” of equipment specified in 2A001.c., 2B001 or 2B003 to 2B009. Note: 2D001 does not control part programming “software” that generates “numerical control” codes for machining various parts. | M3D | SOFTWARE |
| 2D101 | “Software” specially designed or modified for the “use” of equipment specified in 2B104, 2B105, 2B109, 2B116, 2B117 or 2B119 to 2B122. N.B.: SEE ALSO 9D004. | M3D1 | “Software” specially designed or modified for the “use” of “production facilities” and flow-forming machines specified in 3.B.1. or 3.B.3. |
| 2D101 | “Software” specially designed or modified for the “use” of equipment specified in 2B104, 2B105, 2B109, 2B116, 2B117 or 2B119 to 2B122. N.B.: SEE ALSO 9D004. | M6D2 | “Software” specially designed or modified for the equipment specified in 6.B.3., 6.B.4. or 6.B.5. |
| 2D101 | “Software” specially designed or modified for the “use” of equipment specified in 2B104, 2B105, 2B109, 2B116, 2B117 or 2B119 to 2B122. N.B.: SEE ALSO 9D004. | M15D1 | “Software” specially designed or modified for the “use” of equipment specified in 15.B. usable for testing systems specified in 1.A., 19.A.1. or 19.A.2. or subsystems specified in 2.A. or 20.A. |
2E Technology
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 2E001 | “Technology” according to the General Technology Note for the “development” of equipment or “software” specified in 2A, 2B or 2D. Note: 2E001 includes “technology” for the integration of probe systems into coordinate measurement machines specified in 2B006.a. | M | Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
| 2E002 | “Technology” according to the General Technology Note for the “production” of equipment specified in 2A or 2B. | M | Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
| 2E101 | “Technology” according to the General Technology Note for the “use” of equipment or “software” specified in 2B004, 2B009, 2B104, 2B109, 2B116, 2B119 to 2B122 or 2D101. | M | Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
CATEGORY 3 — ELECTRONICS
3A Systems, Equipment and Components
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 3A001 | Electronic components and specially designed components therefor, as follows: a. General purpose integrated circuits, as follows: Note 1: The control status of wafers (finished or unfinished), in which the function has been determined, is to be evaluated against the parameters of 3A001.a. Note 2: Integrated circuits include the following types: — “Monolithic integrated circuits”; — “Hybrid integrated circuits”; — “Multichip integrated circuits”; — “Film type integrated circuits”, including silicon-on-sapphire integrated circuits; — “Optical integrated circuits”; — “Three dimensional integrated circuits”. | ||
| 3A001 | 1. Integrated circuits designed or rated as radiation hardened to withstand any of the following: a. A total dose of 5 × 103 Gy (silicon) or higher; b. A dose rate upset of 5 × 106 Gy (silicon)/s or higher; or c. A fluence (integrated flux) of neutrons (1 MeV equivalent) of 5 × 1013 n/cm2 or higher on silicon, or its equivalent for other materials; Note: 3A001.a.1.c. does not control Metal Insulator Semiconductors (MIS). | M18A1 | “Radiation Hardened”“microcircuits” usable in protecting rocket systems and unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for the systems specified in 1.A. |
| 3A001 | 1. Integrated circuits designed or rated as radiation hardened to withstand any of the following: a. A total dose of 5 × 103 Gy (silicon) or higher; b. A dose rate upset of 5 × 106 Gy (silicon)/s or higher; or c. A fluence (integrated flux) of neutrons (1 MeV equivalent) of 5 × 1013 n/cm2 or higher on silicon, or its equivalent for other materials; Note: 3A001.a.1.c. does not control Metal Insulator Semiconductors (MIS). | M18A2 | ‘Detectors’ specially designed or modified to protect rocket systems and unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for the systems specified in 1.A. Technical Note: 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. |
| 3A101 | Electronic equipment, devices and components, other than those specified in 3A001, as follows: a. Analogue-to-digital converters, usable in “missiles”, designed to meet military specifications for ruggedized equipment; | M14A1 | Analogue-to-digital converters, usable in the systems specified in 1.A., having any of the following characteristics: a) Designed to meet military specifications for ruggedised equipment; or b) Designed or modified for military use and being any of the following types: |
| 3A101 | Electronic equipment, devices and components, other than those specified in 3A001, as follows: a. Analogue-to-digital converters, usable in “missiles”, designed to meet military specifications for ruggedized equipment; | M14A1b1 | 1. Analogue-to-digital converter “microcircuits”, which are “radiation hardened” or have all of the following characteristics: a. Rated for operation in the temperature range from below –54 °C to above +125 °C; and b. Hermetically sealed; or |
| 3A101 | Electronic equipment, devices and components, other than those specified in 3A001, as follows: a. Analogue-to-digital converters, usable in “missiles”, designed to meet military specifications for ruggedized equipment; | M14A1b2 | 2. Electrical input type analogue-to-digital converter printed circuit boards or modules, having all of the following characteristics: a. Rated for operation in the temperature range from below –45 °C to above +80 °C; and b. Incorporating “microcircuits” specified in 14.A.1.b.1. |
| 3A101 | b. Accelerators capable of delivering electromagnetic radiation produced by bremsstrahlung from accelerated electrons of 2 MeV or greater, and systems containing those accelerators. Note: 3A101.b. above does not specify equipment specially designed for medical purposes. | M15B5 | Accelerators capable of delivering electromagnetic radiation produced by bremsstrahlung from accelerated electrons of 2 MeV or greater, and equipment containing those accelerators, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A. or 20.A. Note: 15.B.5. does not control equipment specially designed for medical purposes. Technical Note: In Item 15.B. ‘bare table’ means a flat table, or surface, with no fixture or fittings. |
| 3A102 | ‘Thermal batteries’ designed or modified for ‘missiles’. Technical Notes: 1. In 3A102 ‘thermal batteries’ are single use batteries that contain a solid non-conducting inorganic salt as the electrolyte. These batteries incorporate a pyrolytic material that, when ignited, melts the electrolyte and activates the battery. 2. In 3A102 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. | M12A6 | Thermal batteries designed or modified for the systems specified in 1.A., 19.A.1. or 19.A.2. Note: Item 12.A.6. does not control thermal batteries specially designed for rocket systems or unmanned aerial vehicles that are not capable of a “range” equal to or greater than 300 km. Technical Note: Thermal batteries are single use batteries that contain a solid non-conducting inorganic salt as the electrolyte. These batteries incorporate a pyrolytic material that, when ignited, melts the electrolyte and activates the battery. |
3D Software
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 3D101 | “Software” specially designed or modified for the “use” of equipment specified in 3A101.b. | M15D1 | “Software” specially designed or modified for the “use” of equipment specified in 3A101.b. |
3E Technology
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 3E001 | “Technology” according to the General Technology Note for the “development” or “production” of equipment or materials specified in 3A, 3B or 3C; Note 1: 3E001 does not control “technology” for the “production” of equipment or components controlled by 3A003. Note 2: 3E001 does not control “technology” for the “development” or “production” of integrated circuits specified in 3A001.a.3. to 3A001.a.12., having all of the following: a. Using “technology” at or above 0,130 μm; and b. Incorporating multi-layer structures with three or fewer metal layers. | M | Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
| 3E101 | “Technology” according to the General Technology Note for the “use” of equipment or “software” specified in 3A001.a.1. or 2., 3A101, 3A102 or 3D101. | M | Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
| 3E102 | “Technology” according to the General Technology Note for the “development” of “software” specified in 3D101. | M15E1 | “Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 15.B. or 15.D. |
CATEGORY 4 — COMPUTERS
4A Systems, Equipment and Components
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 4A001 | Electronic computers and related equipment, having any of the following and “electronic assemblies” and specially designed components therefor: N.B.: SEE ALSO 4A101. | ||
| 4A001 | a. Specially designed to have any of the following: 1. Rated for operation at an ambient temperature below 228 K (–45 °C) or above 358 K (85 °C); or Note: 4A001.a.1. does not control computers specially designed for civil automobile, railway train or “civil aircraft” applications. 2. Radiation hardened to exceed any of the following specifications: a. Total Dose 5 × 103 Gy (silicon); b. Dose Rate Upset 5 × 106 Gy (silicon)/s; or c. Single Event Upset 1 × 10–8 Error/bit/day; Note: 4A001.a.2. does not control computers specially designed for “civil aircraft” applications. b. Not used. | M13A1 | Analogue computers, digital computers or digital differential analysers, designed or modified for use in the systems specified in 1.A., having any of the following characteristics: a) Rated for continuous operation at temperatures from below –45 °C to above +55 °C; or b) Designed as ruggedised or “radiation hardened”. |
| 4A003 | “Digital computers”, “electronic assemblies”, and related equipment therefor, as follows and specially designed components therefor: Note 1: 4A003 includes the following: — ‘Vector processors’; — Array processors; — Digital signal processors; — Logic processors; — Equipment designed for “image enhancement”; — Equipment designed for “signal processing”. Note 2: The control status of the “digital computers” and related equipment described in 4A003 is determined by the control status of other equipment or systems provided: a. The “digital computers” or related equipment are essential for the operation of the other equipment or systems; b. The “digital computers” or related equipment are not a “principal element” of the other equipment or systems; and N.B. 1: The control status of “signal processing” or “image enhancement” equipment specially designed for other equipment with functions limited to those required for the other equipment is determined by the control status of the other equipment even if it exceeds the “principal element” criterion. N.B. 2: For the control status of “digital computers” or related equipment for telecommunications equipment, see Category 5, Part 1 (Telecommunications). c. The “technology” for the “digital computers” and related equipment is determined by 4E. d. Not used | ||
| 4A003 | e. Equipment performing analogue-to-digital conversions exceeding the limits specified in 3A001.a.5.; | M14A1b2 | Electrical input type analogue-to-digital converter printed circuit boards or modules, having all of the following characteristics: a) Rated for operation in the temperature range from below –45 °C to above +80 °C; and b) Incorporating “microcircuits” specified in 14.A.1.b.1. |
| 4A101 | Analogue computers, “digital computers” or digital differential analysers, other than those specified in 4A001.a.1., which are ruggedized and designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. | M13A1b | Designed as ruggedised or “radiation hardened”. |
| 4A102 | “Hybrid computers” specially designed for modelling, simulation or design integration of space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. Note: This control only applies when the equipment is supplied with “software” specified in 7D103 or 9D103. | M16A1 | Specially designed hybrid (combined analogue/digital) computers for modelling, simulation or design integration of systems specified in 1.A. or the subsystems specified in 2.A. Note: This control only applies when the equipment is supplied with “software” specified in 16.D.1. |
4E Technology
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 4E001 | a. “Technology” according to the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 4A or 4D. b. “Technology”, other than that specified in 4E001.a., specially designed or modified for the “development” or “production” of equipment as follows: 1. “Digital computers” having an “Adjusted Peak Performance” (“APP”) exceeding 1,0 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 4E001.b.1. c. “Technology” for the “development” of “intrusion software”. | M | Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
CATEGORY 5 — TELECOMMUNICATIONS AND “INFORMATION SECURITY”
Part 1 — Telecommunications
5A1 Systems, Equipment and Components
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 5A101 | Telemetry and telecontrol equipment, including ground equipment, designed or modified for ‘missiles’. Technical Note: In 5A101 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. Note: 5A101 does not control: a. Equipment designed or modified for manned aircraft or satellites; b. Ground based equipment designed or modified for terrestrial or marine applications; c. Equipment designed for commercial, civil or ‘Safety of Life’ (e.g. data integrity, flight safety) GNSS services; | M12A4 | Telemetry and telecontrol equipment, including ground equipment, designed or modified for systems specified in 1.A., 19.A.1. or 19.A.2. Notes: 1. 12.A.4. does not control equipment designed or modified for manned aircraft or satellites. 2. 12.A.4. does not control ground based equipment designed or modified for terrestrial or marine applications. 3. 12.A.4. does not control equipment designed for commercial, civil or ‘Safety of Life’ (e.g. data integrity, flight safety) GNSS services. |
5D1 Software
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 5D101 | “Software” specially designed or modified for the “use” of equipment specified in 5A101. | M12D3 | “Software” specially designed or modified for the “use” of equipment specified in 12.A.4. or 12.A.5., usable for systems specified in 1.A., 19.A.1. or 19.A.2. |
5E1 Technology
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 5E101 | “Technology” according to the General Technology Note for the “development”, “production” or “use” of equipment specified in 5A101. | M12E1 | “Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 12.A. or 12.D. |
CATEGORY 6 — SENSORS AND LASERS
6A Systems, Equipment and Components
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 6A002 | Optical sensors or equipment and components therefor, as follows: N.B.: SEE ALSO 6A102. a. Optical detectors as follows: 1. “Space-qualified” solid-state detectors as follows: Note: For the purpose of 6A002.a.1., solid-state detectors include “focal plane arrays”. a. “Space-qualified” solid-state detectors having all of the following: 1. A peak response in the wavelength range exceeding 10 nm but not exceeding 300 nm; and 2. A response of less than 0,1 % relative to the peak response at a wavelength exceeding 400 nm; | M18A2 | ‘Detectors’ specially designed or modified to protect rocket systems and unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for the systems specified in 1.A. Technical Note: 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 |
| 6A002 | b. “Space-qualified” solid-state detectors having all of the following: 1. A peak response in the wavelength range exceeding 900 nm but not exceeding 1 200 nm; and 2. A response “time constant” of 95 ns or less; c. “Space-qualified” solid-state detectors having a peak response in the wavelength range exceeding 1 200 nm but not exceeding 30 000 nm; d. “Space-qualified”“focal plane arrays” having more than 2 048 elements per array and having a peak response in the wavelength range exceeding 300 nm but not exceeding 900 nm. | M11A2 | Passive sensors for determining bearings to specific electromagnetic sources (direction finding equipment) or terrain characteristics, designed or modified for use in the systems specified in 1.A. |
| 6A006 | “Magnetometers”, “magnetic gradiometers”, “intrinsic magnetic gradiometers”, underwater electric field sensors, “compensation systems”, and specially designed components therefor, as follows: N.B.: SEE ALSO 7A103.d. Note: 6A006 does not control instruments specially designed for fishery applications or biomagnetic measurements for medical diagnostics. a. “Magnetometers” and subsystems as follows: 1. “Magnetometers” using “superconductive” (SQUID) “technology” and having any of the following: a. SQUID systems designed for stationary operation, without specially designed subsystems designed to reduce in-motion noise, and having a ‘sensitivity’ equal to or lower (better) than 50 fT (rms) per square root Hz at a frequency of 1 Hz; or b. SQUID systems having an in-motion-magnetometer ‘sensitivity’ lower (better) than 20 pT (rms) per square root Hz at a frequency of 1 Hz and specially designed to reduce in-motion noise; 2. “Magnetometers” using optically pumped or nuclear precession (proton/Overhauser) “technology” having a ‘sensitivity’ lower (better) than 20 pT (rms) per square root Hz at a frequency of 1 Hz; 3. “Magnetometers” using fluxgate “technology” having a ‘sensitivity’ equal to or lower (better) than 10 pT (rms) per square root Hz at a frequency of 1 Hz; 4. Induction coil “magnetometers” having a ‘sensitivity’ lower (better) than any of the following: a. 0,05 nT (rms) per square root Hz at frequencies of less than 1 Hz; b. 1 × 10–3 nT (rms) per square root Hz at frequencies of 1 Hz or more but not exceeding 10 Hz; or c. 1 × 10–4 nT (rms) per square root Hz at frequencies exceeding 10 Hz; 5. Fibre optic “magnetometers” having a ‘sensitivity’ lower (better) than 1 nT (rms) per square root Hz; b. Underwater electric field sensors having a ‘sensitivity’ lower (better) than 8 nanovolt per metre per square root Hz when measured at 1 Hz; c. “Magnetic gradiometers” as follows: 1. “Magnetic gradiometers” using multiple “magnetometers” specified in 6A006.a.; 2. Fibre optic “intrinsic magnetic gradiometers” having a magnetic gradient field ‘sensitivity’ lower (better) than 0,3 nT/m rms per square root Hz; 3. “Intrinsic magnetic gradiometers”, using “technology” other than fibre-optic “technology”, having a magnetic gradient field ‘sensitivity’ lower (better) than 0,015 nT/m rms per square root Hz; d. “Compensation systems” for magnetic or underwater electric field sensors resulting in a performance equal to or better than the specified parameters of 6A006.a., 6A006.b. or 6A006.c.; | M9A8 | Three axis magnetic heading sensors having all of the following characteristics, and specially designed components therefor: a) Internal tilt compensation in pitch (+/– 90 degrees) and having roll (+/– 180 degrees) axes. b) Capable of providing azimuthal accuracy better (less) than 0,5 degrees rms at latitudes of +/– 80 degrees, referenced to local magnetic field; and c) Designed or modified to be integrated with flight control and navigation systems. Note: Flight control and navigation systems in Item 9.A.8. include gyrostabilisers, automatic pilots and inertial navigation systems. |
| 6A007 | Gravity meters (gravimeters) and gravity gradiometers, as follows: N.B.: SEE ALSO 6A107. a. Gravity meters designed or modified for ground use and having a static accuracy of less (better) than 10 μGal; Note: 6A007.a. does not control ground gravity meters of the quartz element (Worden) type. b. Gravity meters designed for mobile platforms and having all of the following: 1. A static accuracy of less (better) than 0,7 mGal; and 2. An in-service (operational) accuracy of less (better) than 0,7 mGal having a ‘time-to-steady-state registration’ of less than 2 minutes under any combination of attendant corrective compensations and motional influences; Technical Note: For the purposes of 6A007.b., ‘time-to-steady-state registration’ (also referred to as the gravimeter's response time) is the time over which the disturbing effects of platform induced accelerations (high frequency noise) are reduced. c. Gravity gradiometers. | M12A3 | Gravity meters (gravimeters) or gravity gradiometers, designed or modified for airborne or marine use, usable for systems specified in 1.A., as follows, and specially designed components therefor: a) Gravity meters having all the following: 1. A static or operational accuracy equal to or less (better) than 0,7 milligal (mgal); and 2. A time to steady-state registration of two minutes or less; b) Gravity gradiometers. |
| 6A008 | Radar systems, equipment and assemblies, having any of the following, and specially designed components therefor: N.B.: SEE ALSO 6A108. Note: 6A008 does not control: — Secondary surveillance radar (SSR); — Civil Automotive Radar; — Displays or monitors used for air traffic control (ATC); — Meteorological (weather) radar; — Precision approach radar (PAR) equipment conforming to ICAO standards and employing electronically steerable linear (1-dimensional) arrays or mechanically positioned passive antennae. | M11A1 | Radar and laser radar systems, including altimeters, designed or modified for use in the systems specified in 1.A. Technical Note: Laser radar systems embody specialised transmission, scanning, receiving and signal processing techniques for utilisation of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics. |
| 6A008 | a. Operating at frequencies from 40 GHz to 230 GHz and having any of the following: 1. An average output power exceeding 100 mW; or 2. Locating accuracy of 1 m or less (better) in range and 0,2 degree or less (better) in azimuth; b. A tunable bandwidth exceeding ± 6,25 % of the ‘centre operating frequency’; Technical Note: The ‘centre operating frequency’ equals one half of the sum of the highest plus the lowest specified operating frequencies. c. Capable of operating simultaneously on more than two carrier frequencies; | M12A5b | Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities: 1. Angular resolution better than 1,5 mrad; 2. Range of 30 km or greater with a range resolution better than 10 m rms; and 3. Velocity resolution better than 3 m/s. |
| 6A102 | Radiation hardened ‘detectors’, other than those specified in 6A002, specially designed 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 × 105 rads (silicon). Technical Note: In 6A102, 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. | M18A2 | ‘Detectors’ specially designed or modified to protect rocket systems and unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for the systems specified in 1.A. Technical Note: 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. |
| 6A107 | Gravity meters (gravimeters) and components for gravity meters and gravity gradiometers, as follows: a. Gravity meters, other than those specified in 6A007.b, designed or modified for airborne or marine use, and having a static or operational accuracy equal to or less (better) than 0,7 milligal (mgal), and having a time-to-steady-state registration of two minutes or less; b. Specially designed components for gravity meters specified in 6A007.b or 6A107.a. and gravity gradiometers specified in 6A007.c. | M12A3 | Gravity meters (gravimeters) or gravity gradiometers, designed or modified for airborne or marine use, usable for systems specified in 1.A., as follows, and specially designed components therefor: a) Gravity meters having all the following: 1. A static or operational accuracy equal to or less (better) than 0,7 milligal (mgal); and 2. A time to steady-state registration of two minutes or less; b) Gravity gradiometers. |
| 6A108 | Radar systems and tracking systems, other than those specified in entry 6A008, as follows: a. Radar and laser radar systems designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104; Note: 6A108.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. | M11A1 | Radar and laser radar systems, including altimeters, designed or modified for use in the systems specified in 1.A. Technical Note: Laser radar systems embody specialised transmission, scanning, receiving and signal processing techniques for utilisation of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics. |
| 6A108 | 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 1,5 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 6A108.b. ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. | M12A5 | Precision tracking systems, usable for systems specified in 1.A., 19.A.1. or 19.A.2. as follows: a. Tracking systems which use a code translator installed on the rocket or unmanned aerial vehicle in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurements of inflight position and velocity; b. Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities: 1. Angular resolution better than 1,5 mrad; 2. Range of 30 km or greater with a range resolution better than 10 m rms; and 3. Velocity resolution better than 3 m/s. |
6B Test, Inspection and Production Equipment
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 6B008 | Pulse radar cross-section measurement systems having transmit pulse widths of 100 ns or less, and specially designed components therefor. N.B.: SEE ALSO 6B108. | M17B1 | Systems, specially designed for radar cross section measurement, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A |
| 6B108 | Systems, other than those specified in 6B008, specially designed for radar cross section measurement usable for ‘missiles’ and their subsystems. Technical Note: In 6B108 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. | M17B1 | Systems, specially designed for radar cross section measurement, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A |
6D Software
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 6D002 | “Software” specially designed for the “use” of equipment specified in 6A002.b., 6A008 or 6B008. | M | Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
| 6D102 | “Software” specially designed or modified for the “use” of goods specified in 6A108. | M11D1 | “Software” specially designed or modified for the “use” of equipment specified in 11.A.1., 11.A.2. or 11.A.4. |
| 6D102 | “Software” specially designed or modified for the “use” of goods specified in 6A108. | M12D3 | “Software” specially designed or modified for the “use” of equipment specified in 12.A.4. or 12.A.5., usable for systems specified in 1.A., 19.A.1. or 19.A.2. |
| 6D103 | “Software” which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for ‘missiles’. Technical Note: In 6D103 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. | M12D2 | “Software” which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for systems specified in 1.A., 19.A.1. or 19.A.2. |
6E Technology
| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex |
|---|---|---|---|
| 6E001 | “Technology” according to the General Technology Note for the “development” of equipment, materials or “software” specified in 6A, 6B, 6C or 6D. | M | Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
| 6E002 | “Technology” according to the General Technology Note for the “production” of equipment or materials specified in 6A, 6B or 6C. | M | Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
| 6E101 | “Technology” according to the General Technology Note for the “use” of equipment or “software” specified in 6A002, 6A007.b. and c., 6A008, 6A102, 6A107, 6A108, 6B108, 6D102 or 6D103. Note: 6E101 only specifies “technology” for equipment specified in 6A008 when it is designed for airborne applications and is usable in “missiles”. | M | Means specific information which is required for the “development”, “production” or “use” of a product. The information may take the form of “technical data” or “technical assistance”. |
CATEGORY 7 — NAVIGATION AND AVIONICS
7A Systems, Equipment and Components
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