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Beechcraft_King_Air_300-Stall_During_Approach.pdf

The aircraft was above the glide slope and the airspeed was approximately 100 knots indicated airspeed. The normal approach speed is approximately 125 KIAS. The PF began to take corrective action just as the aircraft stalled. The PF initiated a stall recovery by applying maximum power and lowering the aircraft’s nose.

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Beechcraft_King_Air_300-Stall_During_Approach.pdfDownload