Navigate / EASA

CS 27.397  Limit pilot forces and torques

ED Decision 2003/15/RM

(a)     Except as provided in sub-paragraph (b) the limit pilot forces are as follows:

(1)     For foot controls, 578 N (130 lbs).

(2)     For stick controls, 445 N (100 lbs) fore and aft, and 298 N (67 lbs) laterally.

(b)     For flap, tab, stabiliser, rotor brake, and landing gear operating controls, the following apply:

(1)     Crank, wheel, and lever controls, (25.4 + R) x 2.919 N, where R = radius in millimetres (  x 50 lbs, where R = radius in inches), but not less than 222 N (50 lbs) nor more than 445 N (100 lbs) for hand-operated controls or 578 N (130 lbs) for foot-operated controls, applied at any angle within 20° of the plane of motion of the control.

(2)     Twist controls, 356 x R Newton-millimetres, where R = radius in millimetres (80 x R inch-pounds where R = radius in inches).