What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Pilot reported a rough running engine and attempted to make it back to airport, made emergency landing. (.4)about 30 minutes after takeoff, the engine began to run rough and lose power. The first pilot (pilot-in-command) attempted to regain full power and return to the departure airport. The airplane continued to descend and the first pilot attempted to land in a hayfield about four miles from the airport. During the forced landing, which occurred in a tailwind, the pilot noticed power lines ahead. He forced the airplane onto rough terrain beneath the power lines. The airplane nosed over on landing and was substantially damaged. An examination of the engine revealed that the exhaust valve stem on the no. 4 cylinder had separated from the valve head. The fracture surface was obliterated and the mode of failure could not be determined. After the failure of the valve, further damage to other cylinder components subsequently occurred as the engine continued to operate in a degraded condition. The no. 4 cylinder had been reworked about 108 flight hours prior to the accident.
As the FAA filed it
PILOT REPORTED A ROUGH RUNNING ENGINE AND ATTEMPTED TO MAKE IT BACK TO AIRPORT, MADE EMERGENCY LANDING. (.4)ABOUT 30 MINUTES AFTER TAKEOFF, THE ENGINE BEGAN TO RUN ROUGH AND LOSE POWER. THE FIRST PILOT (PILOT-IN-COMMAND) ATTEMPTED TO REGAIN FULL POWER AND RETURN TO THE DEPARTURE AIRPORT. THE AIRPLANE CONTINUED TO DESCEND AND THE FIRST PILOT ATTEMPTED TO LAND IN A HAYFIELD ABOUT FOUR MILES FROM THE AIRPORT. DURING THE FORCED LANDING, WHICH OCCURRED IN A TAILWIND, THE PILOT NOTICED POWER LINES AHEAD. HE FORCED THE AIRPLANE ONTO ROUGH TERRAIN BENEATH THE POWER LINES. THE AIRPLANE NOSED OVER ON LANDING AND WAS SUBSTANTIALLY DAMAGED. AN EXAMINATION OF THE ENGINE REVEALED THAT THE EXHAUST VALVE STEM ON THE NO. 4 CYLINDER HAD SEPARATED FROM THE VALVE HEAD. THE FRACTURE SURFACE WAS OBLITERATED AND THE MODE OF FAILURE COULD NOT BE DETERMINED. AFTER THE FAILURE OF THE VALVE, FURTHER DAMAGE TO OTHER CYLINDER COMPONENTS SUBSEQUENTLY OCCURRED AS THE ENGINE CONTINUED TO OPERATE IN A DEGRADED CONDITION. THE NO. 4 CYLINDER HAD BEEN REWORKED ABOUT 108 FLIGHT HOURS PRIOR TO THE ACCIDENT.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N6844X · 1
Matched to the same aircraft by N-number and date.