Navigate / EASA

CS 22.1149  Propeller speed and pitch controls

ED Decision 2003/13/RM

(a)     Propeller speed and pitch must be limited to values that ensure safe operation under normal operating conditions. In addition -

(1)     If there are propeller speed or pitch controls, their operation must not require undue attention or exceptional skill.

(2)     For variable pitch propellers provisions must be made for a positive indication that

(i)      the allowable pitch range for engine start; and

(ii)     the take-off pitch position has been reached.

(b)     Propellers that cannot be controlled in flight must meet the following requirements:

(1)     during take-off and initial climb at VY, the propeller must limit the engine rotational speed at full throttle to a value not greater than the maximum allowable take-off rotational speed, and

(2)     during a glide at VNE with throttle closed or the engine inoperative, provided this has no detrimental effect on the engine, the propeller must not permit the engine to achieve a rotational speed greater than 110% of the maximum continuous speed.

(3)     For powered sailplanes capable of extending and retracting the powerplant during a glide at VPE with the throttle closed, the propeller must not permit the engine to achieve a rotational speed of more than 110% of the max. continuous speed. VPE must not be less than 1.4 VS1 where VS1 is the stalling speed with the wing flaps neutral at maximum weight.

(c)      A propeller that can be controlled in flight but does not have constant speed controls must be so designed that –

(1)     CS 22.1149(b)(1) is met with the lowest possible pitch selected, and

(2)     CS 22.1149(b)(2) is met with the highest possible pitch selected.

(d)     A controllable pitch propeller with constant speed controls must comply with the following requirements:

(1)     with the governor in operation, there must be a means to limit the maximum engine rotational speed to the maximum allowable take-off speed, and

(2)     with the governor inoperative, there must be a means to limit the maximum engine rotational speed to 103% of the maximum allowable take-off speed with the propeller blades at the lowest possible pitch and the powered sailplane stationary with no wind.