Motion and effect of cockpit controls.

CFR · 2024-01-01 · US · Title 14

Cockpit controls must be designed so that they operate in accordance with the following movements and actuation: (a) Flight controls, including the collective pitch control, must operate with a sense of motion which corresponds to the effect on the rotorcraft. (b) Twist-grip engine power controls must be designed so that, for lefthand operation, the motion of the pilot's hand is clockwise to increase power when the hand is viewed from the edge (c) Normal landing gear controls must operate downward to extend the landing gear.

official document · source cfr-2024 · id 14:§ 29.779