Incident Overview
During the climb-out phase after departure, the pilot encountered a partial loss of engine power. In response, he initiated a return to the runway at the departure airport. However, the aircraft did not have sufficient altitude to complete the maneuver and impacted the ground short of the runway.
Post-Accident Examination
A detailed examination of the wreckage was conducted. Investigators found water present in several fuel system components, including the fuel selector valve, fuel manifold, fuel pump, and one header tank.
Aircraft Maintenance History
According to the pilot, the aircraft had been serviced approximately two to three weeks prior to the accident. Additionally, an annual inspection had been completed on September 2, 1989.
Summary
The accident involved a partial loss of engine power during climb, an attempted return to the departure airport, and a short landing. The presence of water in the fuel system was documented during the wreckage examination.