What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Most power on climbout. Came to rest inverted in sewage pond. Cause power loss not addressed. (.4)the pilot stated that the preflight and run-up were conducted with no anomalies noted. After takeoff, the airplane experienced a loss of engine power followed by a loss of altitude and collision with terrain. The airplane came to rest inverted in a sewage pond near the airport. After the power loss, the pilot made an unsuccessful attempt to restart the engine utilizing the emergency checklist. The engine was inspected and mechanical continuity of the engine was established. The crankcase was separated and it was noted that the bearings, pistons, and cylinders exhibited heat discoloration. The number 4 main bearing exhibited evidence of rubbing on the crankshaft and a section of that bearing insert was severely worn, heat distressed, and had flowed over the edge of the crankcase bearing journal. The number 6 connecting rod bearing insert exhibited an unidentified metal substance in the oil port. The remaining crankcase oil journals were found to be clear. The oil pump was disassembled and revealed a nick on one of the driven gear teeth, which corresponded to circumferential scoring on the oil pump housing. The oil filter and suction screen were clean. No further discrep ancies were noted filter and suction screen were clean. Review of the maintenance reocrds revealed that an annual inspection, which included an oil change, had been completed approximately 1 hour prior to the accidnet flight.
As the FAA filed it
MOST POWER ON CLIMBOUT. CAME TO REST INVERTED IN SEWAGE POND. CAUSE POWER LOSS NOT ADDRESSED. (.4)THE PILOT STATED THAT THE PREFLIGHT AND RUN-UP WERE CONDUCTED WITH NO ANOMALIES NOTED. AFTER TAKEOFF, THE AIRPLANE EXPERIENCED A LOSS OF ENGINE POWER FOLLOWED BY A LOSS OF ALTITUDE AND COLLISION WITH TERRAIN. THE AIRPLANE CAME TO REST INVERTED IN A SEWAGE POND NEAR THE AIRPORT. AFTER THE POWER LOSS, THE PILOT MADE AN UNSUCCESSFUL ATTEMPT TO RESTART THE ENGINE UTILIZING THE EMERGENCY CHECKLIST. THE ENGINE WAS INSPECTED AND MECHANICAL CONTINUITY OF THE ENGINE WAS ESTABLISHED. THE CRANKCASE WAS SEPARATED AND IT WAS NOTED THAT THE BEARINGS, PISTONS, AND CYLINDERS EXHIBITED HEAT DISCOLORATION. THE NUMBER 4 MAIN BEARING EXHIBITED EVIDENCE OF RUBBING ON THE CRANKSHAFT AND A SECTION OF THAT BEARING INSERT WAS SEVERELY WORN, HEAT DISTRESSED, AND HAD FLOWED OVER THE EDGE OF THE CRANKCASE BEARING JOURNAL. THE NUMBER 6 CONNECTING ROD BEARING INSERT EXHIBITED AN UNIDENTIFIED METAL SUBSTANCE IN THE OIL PORT. THE REMAINING CRANKCASE OIL JOURNALS WERE FOUND TO BE CLEAR. THE OIL PUMP WAS DISASSEMBLED AND REVEALED A NICK ON ONE OF THE DRIVEN GEAR TEETH, WHICH CORRESPONDED TO CIRCUMFERENTIAL SCORING ON THE OIL PUMP HOUSING. THE OIL FILTER AND SUCTION SCREEN WERE CLEAN. NO FURTHER DISCREP ANCIES WERE NOTED FILTER AND SUCTION SCREEN WERE CLEAN. REVIEW OF THE MAINTENANCE REOCRDS REVEALED THAT AN ANNUAL INSPECTION, WHICH INCLUDED AN OIL CHANGE, HAD BEEN COMPLETED APPROXIMATELY 1 HOUR PRIOR TO THE ACCIDNET FLIGHT.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.