Flight control systems and servo valves, as follows; designed or modified for use in space launch vehicles specified in 9A004, sounding rockets specified in 9A104 or "missiles".
designed or modified to operate in a vibration environment
> 10 g rms
Sub-entries (3)
7A116.a
Pneumatic, hydraulic, mechanical, electro-optical, or electro-mechanical flight control systems (including fly-by-wire and fly-by-light systems);
7A116.b
Attitude control equipment;
7A116.c
Flight control servo valves designed or modified for the systems specified in 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.
designed or modified to operate in a vibration environment: > 10 g rms
Product Examples
Moog fly-by-wire flight control system for space launcher
Parker Aerospace hydraulic servovalve for missile
Safran attitude control equipment for Ariane
Honeywell electromechanical flight system for sounding rocket
Decontrol note
Les systèmes de contrôle de vol destinés à l’aviation civile ou aux aéronefs commerciaux classiques ne sont pas concernés.
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7A116 - Navigation and Avionics - Annex I - The Trade Hub