Aerodynamic stall and ground impact during training flight

1 fatality • Fort Huachuca, United States of America • Takeoff (climb)

A training flight involving a commercial pilot and an airline transport pilot resulted in a fatal crash following a sudden loss of engine power during takeoff.

What happened

A flight was being conducted for the purpose of an orientation and check flight, with an airline transport pilot (ATP) acting as the pilot flying and a commercial pilot acting as an instructor. Following a standard engine run-up, the aircraft type began its takeoff roll. The crew reported that all engine gauges appeared normal during the initial roll, and the aircraft became airborne once it reached 80 knots.

At an altitude of approximately 350 feet above ground level, the crew experienced a sudden jolt. The commercial pilot noted a sensation of power loss and a lack of responsiveness from the aircraft. In response, the commercial pilot deactivated the boost pumps, while the ATP began a gradual left turn to attempt a return to the departure airport. During this maneuver, the aircraft entered a rapid descent characterized by a nose-low and right-wing-low attitude, eventually impacting the ground.

Eyewitnesses observed the departure and reported that the engine sounded normal until the aircraft reached the end of the runway. At that point, witnesses heard distinct popping sounds followed by engine silence. The aircraft was seen entering a left turn at roughly a 45-degree angle with no audible engine noise before descending rapidly.

Findings

Evidence from the wreckage and witness accounts suggests that the aircraft suffered a total loss of engine power. During the attempt to return to the airfield, the pilot flying failed to maintain adequate airspeed, causing the aircraft to exceed its critical angle of attack. This led to an aerodynamic stall and subsequent impact with the terrain. While investigators noted a discrepancy between the cockpit controls and the fuel shutoff valve positions, this finding was not considered a factor that would have prevented the engine from operating normally.

Probable cause

The aircraft experienced a total loss of engine power during a return maneuver, leading to an aerodynamic stall due to insufficient airspeed.

Frequently asked questions

What happened in the 2014-05-17 Rockwell Shrike Commander 500 accident near Fort Huachuca, United States of America?

A training flight involving a commercial pilot and an airline transport pilot resulted in a fatal crash following a sudden loss of engine power during takeoff.

Were there any fatalities in the 2014-05-17 Rockwell Shrike Commander 500 accident?

The accident was fatal, resulting in 1 fatality.

What aircraft was involved and where did it happen?

The accident on 2014-05-17 involved a Rockwell Shrike Commander 500, registration N40TC, operated by Ponderosa Aviation, at Fort Huachuca, United States of America.

What was the probable cause of the accident?

The aircraft experienced a total loss of engine power during a return maneuver, leading to an aerodynamic stall due to insufficient airspeed.

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