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“Software” specially designed for modelling or simulation of the “guidance sets” specified in 7A117 or for their design integration with the space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. Note: “Software” specified in 7D103 remains controlled when combined with specially designed hardware specified in 4A102.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M16D1Code: 7D103“Software” specially designed for modelling or simulation of the “guidance sets” specified in 7A117 or for their design integration with the space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. Note: “Software” specified in 7D103 remains controlled when combined with specially designed hardware specified in 4A102.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M16D1Code: 7D103c. Integration “software” designed or modified for the equipment specified in 7A103.c. Note: A common form of integration “software” employs Kalman filtering.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9D4Code: 7D102c. Integration “software” designed or modified for the equipment specified in 7A103.c. Note: A common form of integration “software” employs Kalman filtering.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9D4Code: 7D102b. Integration “software” specially designed for the equipment specified in 7A003 or 7A103.a.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9D3*Code: 7D102b. Integration “software” specially designed for the equipment specified in 7A003 or 7A103.a.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9D3*Code: 7D102Integration “software” as follows: a. Integration “software” for the equipment specified in 7A103.b.;
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9D2Code: 7D102Integration “software” as follows: a. Integration “software” for the equipment specified in 7A103.b.;
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9D2Code: 7D102“Software” specially designed or modified for the “use” of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M11D1&2Code: 7D101“Software” specially designed or modified for the “use” of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M11D1&2Code: 7D101“Software” specially designed or modified for the “use” of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M10D1Code: 7D101“Software” specially designed or modified for the “use” of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M10D1Code: 7D101“Software” specially designed or modified for the “use” of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M9D1Code: 7D101“Software” specially designed or modified for the “use” of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M9D1Code: 7D101“Software” specially designed or modified for the “use” of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2DCode: 7D101“Software” specially designed or modified for the “use” of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2DCode: 7D101“Source code” for the operation or maintenance of any inertial navigation equipment, including inertial equipment not specified in 7A003 or 7A004, or Attitude and Heading Reference Systems (‘AHRS’). Note: 7D002 does not control “source code” for the “use” of gimballed ‘AHRS’. Technical Note: ‘AHRS’ generally differ from Inertial Navigation Systems (INS) in that an ‘AHRS’ provides attitude and heading information and normally does not provide the acceleration, velocity and position information associated with an INS.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9D1Code: 7D002“Source code” for the operation or maintenance of any inertial navigation equipment, including inertial equipment not specified in 7A003 or 7A004, or Attitude and Heading Reference Systems (‘AHRS’). Note: 7D002 does not control “source code” for the “use” of gimballed ‘AHRS’. Technical Note: ‘AHRS’ generally differ from Inertial Navigation Systems (INS) in that an ‘AHRS’ provides attitude and heading information and normally does not provide the acceleration, velocity and position information associated with an INS.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9D1Code: 7D002“Source code” for the operation or maintenance of any inertial navigation equipment, including inertial equipment not specified in 7A003 or 7A004, or Attitude and Heading Reference Systems (‘AHRS’). Note: 7D002 does not control “source code” for the “use” of gimballed ‘AHRS’. Technical Note: ‘AHRS’ generally differ from Inertial Navigation Systems (INS) in that an ‘AHRS’ provides attitude and heading information and normally does not provide the acceleration, velocity and position information associated with an INS.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M2D3Code: 7D002“Source code” for the operation or maintenance of any inertial navigation equipment, including inertial equipment not specified in 7A003 or 7A004, or Attitude and Heading Reference Systems (‘AHRS’). Note: 7D002 does not control “source code” for the “use” of gimballed ‘AHRS’. Technical Note: ‘AHRS’ generally differ from Inertial Navigation Systems (INS) in that an ‘AHRS’ provides attitude and heading information and normally does not provide the acceleration, velocity and position information associated with an INS.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M2D3Code: 7D002Equipment specially designed for the “production” of equipment specified in 7A. Note: 7B003 includes: — Gyro tuning test stations; — Gyro dynamic balance stations; — Gyro run-in/motor test stations; — Gyro evacuation and fill stations; — Centrifuge fixtures for gyro bearings; — Accelerometer axis align stations; — Fibre optic gyro coil winding machines.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M9B1Code: 7B103Equipment specially designed for the “production” of equipment specified in 7A. Note: 7B003 includes: — Gyro tuning test stations; — Gyro dynamic balance stations; — Gyro run-in/motor test stations; — Gyro evacuation and fill stations; — Centrifuge fixtures for gyro bearings; — Accelerometer axis align stations; — Fibre optic gyro coil winding machines.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M9B1Code: 7B103b. “Production equipment”, and other test, calibration and alignment equipment, other than that specified in 7B001 to 7B003, designed or modified to be used with equipment specified in 7A.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2B2*Code: 7B103b. “Production equipment”, and other test, calibration and alignment equipment, other than that specified in 7B001 to 7B003, designed or modified to be used with equipment specified in 7A.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2B2*Code: 7B103a. “Production facilities” specially designed for equipment specified in 7A117;
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2B1Code: 7B103a. “Production facilities” specially designed for equipment specified in 7A117;
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2B1Code: 7B103Reflectometers specially designed to characterise mirrors, for “laser” gyros, having a measurement accuracy of 50 ppm or less (better).
Authority: EUProhibited Supply To: IRProgram: IREU Code: M9B1Code: 7B102Reflectometers specially designed to characterise mirrors, for “laser” gyros, having a measurement accuracy of 50 ppm or less (better).
Authority: EUProhibited Supply To: IRProgram: IREU Code: M9B1Code: 7B102Equipment specially designed for the “production” of equipment specified in 7A. Note: 7B003 includes: — Gyro tuning test stations; — Gyro dynamic balance stations; — Gyro run-in/motor test stations; — Gyro evacuation and fill stations; — Centrifuge fixtures for gyro bearings; — Accelerometer axis align stations; — Fibre optic gyro coil winding machines.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9B1Code: 7B003Equipment specially designed for the “production” of equipment specified in 7A. Note: 7B003 includes: — Gyro tuning test stations; — Gyro dynamic balance stations; — Gyro run-in/motor test stations; — Gyro evacuation and fill stations; — Centrifuge fixtures for gyro bearings; — Accelerometer axis align stations; — Fibre optic gyro coil winding machines.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9B1Code: 7B003Equipment specially designed for the “production” of equipment specified in 7A. Note: 7B003 includes: — Gyro tuning test stations; — Gyro dynamic balance stations; — Gyro run-in/motor test stations; — Gyro evacuation and fill stations; — Centrifuge fixtures for gyro bearings; — Accelerometer axis align stations; — Fibre optic gyro coil winding machines.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M2B2Code: 7B003Equipment specially designed for the “production” of equipment specified in 7A. Note: 7B003 includes: — Gyro tuning test stations; — Gyro dynamic balance stations; — Gyro run-in/motor test stations; — Gyro evacuation and fill stations; — Centrifuge fixtures for gyro bearings; — Accelerometer axis align stations; — Fibre optic gyro coil winding machines.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M2B2Code: 7B003Equipment specially designed to characterize mirrors for ring “laser” gyros, as follows: N.B.: SEE ALSO 7B102. a. Scatterometers having a measurement accuracy of 10 ppm or less (better); b. Profilometers having a measurement accuracy of 0,5 nm (5 angstrom) or less (better).
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9B1Code: 7B002Equipment specially designed to characterize mirrors for ring “laser” gyros, as follows: N.B.: SEE ALSO 7B102. a. Scatterometers having a measurement accuracy of 10 ppm or less (better); b. Profilometers having a measurement accuracy of 0,5 nm (5 angstrom) or less (better).
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9B1Code: 7B002Test, calibration or alignment equipment, specially designed for equipment specified in 7A. Note: 7B001 does not control test, calibration or alignment equipment for ‘Maintenance Level I’ or ‘Maintenance Level II’. Technical Notes: 1. ‘Maintenance Level I’ The failure of an inertial navigation unit is detected on the aircraft by indications from the Control and Display Unit (CDU) or by the status message from the corresponding sub-system. By following the manufacturer's manual, the cause of the failure may be localised at the level of the malfunctioning Line Replaceable Unit (LRU). The operator then removes the LRU and replaces it with a spare. 2. ‘Maintenance Level II’ The defective LRU is sent to the maintenance workshop (the manufacturer's or that of the operator responsible for level II maintenance). At the maintenance workshop, the malfunctioning LRU is tested by various appropriate means to verify and localise the defective Shop Replaceable Assembly (SRA) module responsible for the failure. This SRA is removed and replaced by an operative spare. The defective SRA (or possibly the complete LRU) is then shipped to the manufacturer. ‘Maintenance Level II’ does not include the disassembly or repair of controlled accelerometers or gyro sensors.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M10B1Code: 7B001Test, calibration or alignment equipment, specially designed for equipment specified in 7A. Note: 7B001 does not control test, calibration or alignment equipment for ‘Maintenance Level I’ or ‘Maintenance Level II’. Technical Notes: 1. ‘Maintenance Level I’ The failure of an inertial navigation unit is detected on the aircraft by indications from the Control and Display Unit (CDU) or by the status message from the corresponding sub-system. By following the manufacturer's manual, the cause of the failure may be localised at the level of the malfunctioning Line Replaceable Unit (LRU). The operator then removes the LRU and replaces it with a spare. 2. ‘Maintenance Level II’ The defective LRU is sent to the maintenance workshop (the manufacturer's or that of the operator responsible for level II maintenance). At the maintenance workshop, the malfunctioning LRU is tested by various appropriate means to verify and localise the defective Shop Replaceable Assembly (SRA) module responsible for the failure. This SRA is removed and replaced by an operative spare. The defective SRA (or possibly the complete LRU) is then shipped to the manufacturer. ‘Maintenance Level II’ does not include the disassembly or repair of controlled accelerometers or gyro sensors.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M10B1Code: 7B001Test, calibration or alignment equipment, specially designed for equipment specified in 7A. Note: 7B001 does not control test, calibration or alignment equipment for ‘Maintenance Level I’ or ‘Maintenance Level II’. Technical Notes: 1. ‘Maintenance Level I’ The failure of an inertial navigation unit is detected on the aircraft by indications from the Control and Display Unit (CDU) or by the status message from the corresponding sub-system. By following the manufacturer's manual, the cause of the failure may be localised at the level of the malfunctioning Line Replaceable Unit (LRU). The operator then removes the LRU and replaces it with a spare. 2. ‘Maintenance Level II’ The defective LRU is sent to the maintenance workshop (the manufacturer's or that of the operator responsible for level II maintenance). At the maintenance workshop, the malfunctioning LRU is tested by various appropriate means to verify and localise the defective Shop Replaceable Assembly (SRA) module responsible for the failure. This SRA is removed and replaced by an operative spare. The defective SRA (or possibly the complete LRU) is then shipped to the manufacturer. ‘Maintenance Level II’ does not include the disassembly or repair of controlled accelerometers or gyro sensors.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9B1Code: 7B001Test, calibration or alignment equipment, specially designed for equipment specified in 7A. Note: 7B001 does not control test, calibration or alignment equipment for ‘Maintenance Level I’ or ‘Maintenance Level II’. Technical Notes: 1. ‘Maintenance Level I’ The failure of an inertial navigation unit is detected on the aircraft by indications from the Control and Display Unit (CDU) or by the status message from the corresponding sub-system. By following the manufacturer's manual, the cause of the failure may be localised at the level of the malfunctioning Line Replaceable Unit (LRU). The operator then removes the LRU and replaces it with a spare. 2. ‘Maintenance Level II’ The defective LRU is sent to the maintenance workshop (the manufacturer's or that of the operator responsible for level II maintenance). At the maintenance workshop, the malfunctioning LRU is tested by various appropriate means to verify and localise the defective Shop Replaceable Assembly (SRA) module responsible for the failure. This SRA is removed and replaced by an operative spare. The defective SRA (or possibly the complete LRU) is then shipped to the manufacturer. ‘Maintenance Level II’ does not include the disassembly or repair of controlled accelerometers or gyro sensors.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M9B1Code: 7B001Test, calibration or alignment equipment, specially designed for equipment specified in 7A. Note: 7B001 does not control test, calibration or alignment equipment for ‘Maintenance Level I’ or ‘Maintenance Level II’. Technical Notes: 1. ‘Maintenance Level I’ The failure of an inertial navigation unit is detected on the aircraft by indications from the Control and Display Unit (CDU) or by the status message from the corresponding sub-system. By following the manufacturer's manual, the cause of the failure may be localised at the level of the malfunctioning Line Replaceable Unit (LRU). The operator then removes the LRU and replaces it with a spare. 2. ‘Maintenance Level II’ The defective LRU is sent to the maintenance workshop (the manufacturer's or that of the operator responsible for level II maintenance). At the maintenance workshop, the malfunctioning LRU is tested by various appropriate means to verify and localise the defective Shop Replaceable Assembly (SRA) module responsible for the failure. This SRA is removed and replaced by an operative spare. The defective SRA (or possibly the complete LRU) is then shipped to the manufacturer. ‘Maintenance Level II’ does not include the disassembly or repair of controlled accelerometers or gyro sensors.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M2B2Code: 7B001Test, calibration or alignment equipment, specially designed for equipment specified in 7A. Note: 7B001 does not control test, calibration or alignment equipment for ‘Maintenance Level I’ or ‘Maintenance Level II’. Technical Notes: 1. ‘Maintenance Level I’ The failure of an inertial navigation unit is detected on the aircraft by indications from the Control and Display Unit (CDU) or by the status message from the corresponding sub-system. By following the manufacturer's manual, the cause of the failure may be localised at the level of the malfunctioning Line Replaceable Unit (LRU). The operator then removes the LRU and replaces it with a spare. 2. ‘Maintenance Level II’ The defective LRU is sent to the maintenance workshop (the manufacturer's or that of the operator responsible for level II maintenance). At the maintenance workshop, the malfunctioning LRU is tested by various appropriate means to verify and localise the defective Shop Replaceable Assembly (SRA) module responsible for the failure. This SRA is removed and replaced by an operative spare. The defective SRA (or possibly the complete LRU) is then shipped to the manufacturer. ‘Maintenance Level II’ does not include the disassembly or repair of controlled accelerometers or gyro sensors.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M2B2Code: 7B001