Event Description
The accident occurred when the aircraft lost engine power at approximately 200 feet above ground level (AGL) during takeoff. Earlier, the pilot had aborted a previous takeoff attempt because the engine power went to idle despite the throttle being open. After a run-up of about 30 seconds, the pilot decided to try again. During the second takeoff, the power loss recurred at about 200 ft AGL. The pilot attempted to execute a 180-degree turn. During this maneuver, the aircraft's horizontal stabilizer caught a tree limb near the runway, and the aircraft subsequently struck the ground hard on the right main landing gear.
Preflight and Fuel System
The aircraft had not been topped off with fuel after its previous flight. The right fuel tank had been capped at some point to prevent leaking, which prevented fuel samples from being taken from that tank during the preflight inspection. Prior to the accident flight, ten gallons of fuel were added to each tank. The fuel tank selector was positioned on the right tank for takeoff. After the accident, an examination of the fuel system revealed no water or contaminants.
Investigation
The investigation into the engine malfunction found no mechanical reason for the power loss. No water or contaminants were detected in the fuel system. The aircraft had not flown since October 1982 prior to the accident flight.