Rudder pedal adjustment system

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

244 86, 74479, 74561, B64C 1304, B64C 1330

Patent

active

041924762

ABSTRACT:
A mechanism for positioning an aircraft rudder and brake pedal to accommodate the pilot. The present invention provides a means whereby aircraft rudder and brake cables adjustments are not disturbed when the assembly is repositioned anywhere within the adjustment range of the aircraft.

REFERENCES:
patent: 1290280 (1919-01-01), Miller
patent: 1919520 (1933-07-01), Laddon et al.
patent: 2002006 (1935-05-01), Hall
patent: 3129605 (1964-04-01), Bonnel, Jr. et al.

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