(b) Each lift and drag device control must be designed and located to make inadvertent operation improbable. Lift and drag devices intended for ground operation only must have means to prevent the inadvertant operation of their controls in flight if that operation could be hazardous.
(c) The rate of motion of the surfaces in response to the operation of the control and the characteristics of the automatic positioning or load limiting device must give satisfactory flight and performance characteristics under steady or changing conditions of airspeed, engine power, and airplane attitude.
(d) The lift device control must be designed to retract the surfaces from the fully extended position, during steady flight at maximum continuous engine power at any speed below V
[Amdt. 25–23, 35 FR 5675, Apr. 8, 1970, as amended by Amdt. 25–46, 43 FR 50595, Oct. 30, 1978; Amdt. 25–57, 49 FR 6848, Feb. 23, 1984]