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Printed page 2. PDF page 2.
vibrations and possibly sparks from the engine's exhaust. The airplane was equipped with an autofeather system. Since the left propeller was not found in the feathered position, it is unlikely that the left engine stopped producing power but, rather, continuedOpen final report at PDF page 2CEN25FA006: UAS Transervices Inc.: N130GP
Printed page 7. PDF page 7.
minimum controllable airspeed (Vmca) was 94 KCAS. The airplane was equipped with an autofeather system, which automated the feathering of the propeller blades when the system sensed that engine torquemeter oil pressure dropped below 6.5 psi and the power settingOpen final report at PDF page 7CEN25FA006: UAS Transervices Inc.: N130GP
Printed page 10. PDF page 10.
directional control and promptly complete the applicable immediate action items...If the Autofeather system fails, the Captain must positively identify the failed engine immediately and feather the appropriate propeller. It should be noted that [minimum control speed] increOpen final report at PDF page 10CEN25FA006: UAS Transervices Inc.: N130GP