Event Summary
The pilot reported that after takeoff, at an altitude of approximately 150 feet above the runway, the engine experienced a total loss of power. The pilot also noted that a clear liquid sprayed from the upper cowling onto the windscreen. In response, the pilot aborted the takeoff, landed on the remaining runway, but was unable to stop before reaching the end. The airplane skidded off the runway and impacted the airport perimeter fence, resulting in substantial damage to both wings.
Examination Findings
During a postaccident examination, the cowling was removed and the electric fuel pump was actuated. Fuel was observed leaking from the fuel input line fitting at the fuel flow divider. Further examination revealed that the torque strip had been disturbed and the fuel line B-Nut was found to be loose. After the B-Nut was tightened, no fuel leaks were observed.
Maintenance Review
A review of the airplane's engine maintenance log indicated that no recent maintenance had been performed involving the fuel pump, fuel flow divider, or associated fuel lines.