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Printed page 7. PDF page 7.
According to the airplane flight manual, the wings-level aerodynamic stall speed was 87 KCAS with engine power at idle, flaps fully retracted, and an operating weight of 9,000 lbs. The airplane's minimum controllable airspeed (Vmca) was 94 KCAS. The airplaneOpen final report at PDF page 7CEN25FA006: UAS Transervices Inc.: N130GP
Printed page 1. PDF page 1.
85 kts ground speed. The airplane's wings level, no-flap aerodynamic stall speed was 87 kts calibrated airspeed (KCAS), and its single-engine minimum controllable airspeed was 89 KCAS. Recorded weather information for the airport about the time of the accident includedOpen final report at PDF page 1CEN25FA006: UAS Transervices Inc.: N130GP