R22 - Structure, transmissions, rotor and equipment, normal and abnormal operation of systems
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On the R-22 the engine output shaft transmits power to the upper sheave:
When operating at high density altitudes, governor response rate:
Below what rotor RPM can irrecoverable blade stalling occur at 6000’ altitude?
The primary structure of the fuselage is:
R-22 engine Maximum continuous rating:
The main gearbox overtemp light is actuated by a temperature switch located:
Below what rotor RPM can irrecoverable blade stalling occur at sea level?
The fuel gages located on the panel and the low fuel warning light are operated electrically by:
