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You are here: home->amp->R05->R.8.9.2.6.A.1
8926
The low pitch stop on a constant speed propeller is usually set so that
| | A) maximum allowable engine RPM cannot be exceeded with any combination of manifold pressure, altitude, or forward speed. |
| | B) the limiting engine manifold pressure cannot be exceeded with any combination of throttle opening, altitude, or forward speed. |
| | C) the engine will turn at its rated takeoff RPM at sea level when the throttle is opened to allowable takeoff manifold pressure. |
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