ED Decision 2003/16/RM
For rotorcraft with wheel-type landing gear, a braking device must be installed that is:
(a) Controllable by the pilot;
(b) Usable during power-off landings; and
(c) Adequate to:
(1) Counteract any normal unbalanced torque when starting or stopping the rotor; and
(2) Hold the rotorcraft parked on a 10° slope on a dry, smooth pavement.
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