Accident Description
The airplane was substantially damaged during a forced landing following a loss of engine power after takeoff. The pilot stated that while climbing through an altitude of 300 feet above ground level, there was an abrupt loss of engine power without any backfiring. After the power loss, the pilot reportedly switched fuel tanks, confirmed the electric fuel pump switch was on, and confirmed that the magnetos switch was in the both position.
Impact and Damage
The airplane then impacted a down sloping wooded area, severing both wings and stabilizer surfaces from the airplane. Subsequent inspection of the cockpit noted that the flap handle was in the 0 degree flap position, the ignition switch was in the both position, and the fuel selector was on the left fuel tank.
Wreckage Examination
Examination of the wreckage revealed the presence of fuel within the lines leading to the engine driven pump, cylinder compression, engine continuity, and electrical continuity of the ignition system. No anomalies were noted with the engine driven fuel pump and servo.
Pilot Actions
The pilot stated that he did not recall draining the fuel sumps before the flight, which is a listed preflight checklist item for the airplane.