Accident Event
During the initial climb, the engine lost power. The pilot was unable to maintain altitude and performed a forced landing. During this landing, the aircraft collided with a freeway guardrail.
Investigation Findings
Post-accident investigation disclosed a blockage in the fuel inlet screen. The blockage was identified as a small piece of rubber hose interliner.
Maintenance Records
Records indicate that the fuel hose was fabricated and installed on the aircraft on or about January 19, 1990, approximately 38 tach hours prior to the accident. Additionally, the engine had been major overhauled on December 12, 1989, at which time all fuel, oil, and hydraulic hoses were replaced.