Text in force at CAR3R-8: from CAR3R-0, effective 15 May 1956. OCR text
constant speed controls.
(a) Suitable means shall be provided at. the governor to limit the speed of the propeller. Such means shall limit the maximum governed engine speed to a value not exceeding its maximum permissible take-off revolutions per minute.
(b) The low pitch blade stop, or other means incorporated in the propeller mechanism to restrict the pitch range, shall limit the speed of the engine to a value not exceeding 103 percent of the maximum permissible take-off revolutions per minute under the following conditions:
(1) Propeller blades set in the lowest possible pitch and the governor inoperative.
(2) Engine operating at take-off manifold pressure with the airplane stationary and with no wind.