1 fatality

1996-09-09: Rockwell Grand Commander 680 (N262X) — Robert D. Simpson — Lakeland, United States of America

Lakeland, United States of AmericaTakeoff (climb)

On September 9, 1996, a Rockwell Grand Commander 680 (registration N262X) operated by Robert D. Simpson was involved in an aviation accident near Lakeland, United States of America during takeoff. One person was killed. Investigators recorded the probable cause as: Failure of the pilot to maintain minimum control speed, while returning to the airport for a precautionary landing, following a reported loss of power in one engine, which resulted in a loss of aircraft control and an uncontrolled collision with the terrain. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781206719Data APIEditorial standards

After takeoff, a pilot reported losing power in one engine. During a turn back to the airport, the aircraft stalled and crashed on a taxiway. Investigation found no preimpact mechanical failure.

Accident Sequence

After takeoff, the pilot transmitted to air traffic controllers that he had lost power in an engine. He made a steep left turn back toward the airport, then a right turn toward the runway. During the right turn, the aircraft's nose dropped, and the aircraft crashed nose-first on a taxiway.

Post-Crash Examination

Post-crash examination of the aircraft structure and flight control systems revealed no preimpact failure or malfunction. The left propeller was found in the feathered position, and the right propeller was found in a high blade angle. The right propeller had damage consistent with the engine operating. Teardown examination of the engines and propellers showed no findings that would have resulted in engine or propeller malfunction or failure.

Pilot Experience

At the time the aircraft was purchased by the pilot in March 1996, he had not flown for about 10 years. Since purchasing the aircraft, he had logged 2.5 hours of transition/checkout in the airplane and had flown it for a total of about 22 hours, mostly on sightseeing flights.

Probable Cause

The official probable cause was the failure of the pilot to maintain minimum control speed, while returning to the airport for a precautionary landing, following a reported loss of power in one engine, which resulted in a loss of aircraft control and an uncontrolled collision with the terrain. Factors relating to the accident were: loss of power in the left engine for undetermined reason(s), and the pilot's apparent lack of familiarity with single engine operation in the make and model of aircraft.