CS 22.155 Elevator control force in manoeuvres

• ED Decision 2003/13/RM found in: Sailplane Rule Book - Part-SAO Part-SFCL CS-22 (Nov 2022)

CS 22.155 Elevator control force in manoeuvres ED Decision 2003/13/RM 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 VS1 must be 0.5 daN, with the controls trimmed to maintain the sailplane in equilibrium at 1.4 VS1 in steady straight flight with wing-flaps in the most critical position, air brakes and, where applicable, landing gear retracted.