ED Decision 2003/18/RM
(a) Each wing flap control must be designed so that, when the flap has been placed position upon which compliance with the performance requirements is based, the flap will not splice, and pulley used move from that position unless the control is adjusted or is moved by the automatic operation of a flap load limiting device
(b) The rate of movement of the flaps in response to the operation of the pilot’s control or automatic device must give satisfactory flight and performance characteristics under steady or changing conditions of airspeed, engine power, and attitude.
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