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Monticello, UT
DURING CRUISE FLIGHT, ABOUT 5 MIN AFTER PASSING THE MONTICELLO AIRPORT, THE ENGINE BEGAN RUNNING ROUGH. THE PILOT REVERSED COURSE TO RETURN TO THE AIRPORT FOR A PRECAUTIONARY LANDING. AS HE WAS TURNING ONTO BASE LEG, THE ENGINE STOPPED RUNNING. SUBSEQUENTLY, THE AIRCRAFT WAS DAMAGED DURING A FORCED LANDING ABOUT 50 YARDS SHORT OF THE RUNWAY. AN EXAM OF THE ENGINE REVEALED THERE WAS NO OIL IN THE CRANKCASE, A HOLE WAS BURNED IN THE #5 PISTON FROM PRE-IGNITION/DETONATION, THERE WAS EVIDENCE OF ARCING OF THE LEFT MAG AND CONTAMINATION IN THE RIGHT MAG, AND THE FUEL SYSTEM WAS IMPROPERLY ADJUSTED. THE ACFT HAD 88 HOURS OF FLIGHT TIME, SINCE A MAJOR OVERHAUL OF THE ENGINE WAS COMPLETED ON 7/12/91.
INADEQUATE MAINTENANCE/OVERHAUL OF THE ENGINE, AND SUBSEQUENT FAILURE OF THE #5 PISTON (HOLE BURNED IN PISTON), DUE TO PRE-IGNITION AND/OR DETONATION. ROUGH/UNEVEN TERRAIN IN THE EMERGENCY LANDING AREA WAS A RELATED FACTOR.
DURING CRUISE FLIGHT, ABOUT 5 MIN AFTER PASSING THE MONTICELLO AIRPORT, THE ENGINE BEGAN RUNNING ROUGH. THE PILOT REVERSED COURSE TO RETURN TO THE AIRPORT FOR A PRECAUTIONARY LANDING. AS HE WAS TURNING ONTO BASE LEG, THE ENGINE STOPPED RUNNING. SUBSEQUENTLY, THE AIRCRAFT WAS DAMAGED DURING A FORCED LANDING ABOUT 50 YARDS SHORT OF THE RUNWAY. AN EXAM OF THE ENGINE REVEALED THERE WAS NO OIL IN THE CRANKCASE, A HOLE WAS BURNED IN THE #5 PISTON FROM PRE-IGNITION/DETONATION, THERE WAS EVIDENCE OF ARCING OF THE LEFT MAG AND CONTAMINATION IN THE RIGHT MAG, AND THE FUEL SYSTEM WAS IMPROPERLY ADJUSTED. THE ACFT HAD 88 HOURS OF FLIGHT TIME, SINCE A MAJOR OVERHAUL OF THE ENGINE WAS COMPLETED ON 7/12/91.