What happened
The pilot reported that shortly after departing from runway 26, he noticed the engine was not producing sufficient power. In response to this mechanical issue, he executed a 180-degree turn and attempted to land on runway 8. During the landing roll, he estimated a tailwind velocity of approximately 5 knots. The pilot lost directional control of the aircraft, causing it to skid to the left and depart the paved surface.
The investigation
Following the incident, the engine was removed and disassembled for a detailed examination. Mechanics discovered that the number 6 intake valve was burnt and failing to seat properly. This mechanical defect was identified as the direct cause of the power loss experienced during flight.
Findings
The primary factor contributing to the accident was the fuel system component failure, specifically the burnt intake valve which led to inadequate engine performance. The pilot's inability to maintain directional control resulted in the aircraft leaving the runway and sustaining damage to the right rear spar.