CS 22.155  Elevator control force in manoeuvres

CAA ORS9 Decision No. 1

The elevator control forces during turns or when recovering from manoeuvres must be such that an increase in load factor causes an increase in control force. The minimum value of this force for a stabilized turn with a 45° bank at 1.4 V_S1 must be 0.5 daN, with the controls trimmed to maintain the sailplane in equilibrium at 1.4 V_S1 in steady straight flight with wing-flaps in the most critical position, air brakes and, where applicable, landing gear retracted.