A pedal mechanism (100) for an aircraft, the pedal mechanism (100) comprising: a pedal arm (106, 106A) connectable to a pedal (120, 120A) at a pedal connection point (116, 116A), the pedal arm (106, 106A) rotatable about a pedal arm rotation point (108, 108A) on translation of the pedal (119); and a stature adjustment mechanism, the stature adjustment mechanism actuatable, during a stature adjustment process, to move the pedal arm rotation point (108, 108A).
PEDAL MECHANISM
PEDALMECHANISMUS
MÉCANISME DE PÉDALE
2024-05-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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