Accident Overview
While operating in cruise flight, the airplane's engine lost power. The pilot executed a forced landing in a field, during which the aircraft collided with a ditch. No further details about the phase of flight or environmental conditions were provided.
Postaccident Examination
Following the accident, FAA inspectors examined the aircraft. Their inspection determined that the throttle linkage had become disconnected from the fuel control unit. The disconnection was attributed to excessive wear of the linkage connection point.
Maintenance History
The aircraft had received a 100-hour inspection 11 days before the accident. In the intervening period, the aircraft accumulated approximately 8 flight hours. The relationship between the recent inspection and the discovered wear was not specified in the source.