Document ID: chunk:federal_register_of_legislation:F2024L01024:front:0:p224
Version: federal_register_of_legislation:F2024L01024
Segment Type: other
Provision Reference: 
Character Range: 640461–643377

1. Capable of providing navigation information at speeds in excess of 600 m/s;
2. Employing decryption, designed or modified for military or governmental services, to gain access to GNSS secured signal/data; or
3. Being specially designed to employ anti‑jam features (e.g. null steering antenna or electronically steerable antenna) to function in an environment of active or passive countermeasures.
Note: 7A105.b.2. and 7A105.b.3. do not apply to equipment designed for commercial, civil or 'Safety of Life' (e.g., data integrity, flight safety) GNSS services.
7. A. 106. Altimeters, other than those specified by 7A006, of radar or laser radar type, designed or modified for use in space launch vehicles specified by 9A004 or sounding rockets specified by 9A104.
7. A. 115. Passive sensors for determining bearing to specific electromagnetic source (direction finding equipment) or terrain characteristics, designed or modified for use in space launch vehicles specified by 9A004 or sounding rockets specified by 9A104.
Note: 7A115 includes sensors for the following equipment:
a. Terrain contour mapping equipment;
b. Scene mapping and correlation (both digital and analogue) equipment;
c. Doppler navigation radar equipment;
d. Passive interferometer equipment;
e. Imaging sensor equipment (both active and passive).
7. A. 116. Flight control systems and servo valves, as follows; designed or modified for use in space launch vehicles specified by 9A004 or sounding rockets specified by 9A104.
a. Pneumatic, hydraulic, mechanical, electro‑optical, or electromechanical flight control systems (including fly‑by‑wire and fly‑by‑light systems);
b. Attitude control equipment;
7. A. 116. c. Flight control servo valves designed or modified for the systems specified by 7A116.a. or 7A116.b., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz.
7. A. 117. "Guidance sets", usable in "missiles" capable of achieving system accuracy of 3.33% or less of the range (e.g., a 'CEP' of 10 km or less at a range of 300 km).
Note: In 7A117, 'CEP' (Circular Error Probable or Circle of Equal Probability) is a measure of accuracy, defined as the radius of the circle centred at the target, at a specific range, in which 50% of the payloads impact.
7. B.  Test, Inspection and Production Equipment
7. B. 001. Test, calibration or alignment equipment, specially designed for equipment specified by 7A.
Note: 7B001 does not apply to test, calibration or alignment equipment for 'Maintenance Level I' or 'Maintenance Level II'.
Technical Notes:
For the purposes of 7B001.:
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