What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Lost power during a spray run turn around. Hit ditch landing. Found broken crankshaft. Recent top overhaul. (.4)according to the pilot, a loss of engine power occurred, while he was applying insecticide to a farm. A force landing was made in a plowed field. During the landing, the airplane encountered a small ditch in soft terrain, and the airplane nosed over. Examination of the maintenance records revealed that a top overhaul of the engine had been accomplished, 7 days before the accident. Postaccident examination of the engine revealed a fractured crankshaft. Multiple origin sites of the fracture were found from the surface of the journal radius. There was evidence that inadequate torque had been applied to the crankcase through-bolts. The #2 main bearing had moved fore and aft in the bearing bore and had rotated in the crankcase; there was heavy fretting at the #2 and #3 main bearing boss parting surfaces; and there was evidence of severe pounding from lack of support that had started a breakup of the #2 bearing. (-23) the spray pilot was in a maneuvering turn when the engine lost power. The pilot made an emergency landing in a soft plowed field. Hitting a small ditch the plane flipped over causing substantial damage. The pilot exited the airplane through a side window with no injuries.
As the FAA filed it
LOST POWER DURING A SPRAY RUN TURN AROUND. HIT DITCH LANDING. FOUND BROKEN CRANKSHAFT. RECENT TOP OVERHAUL. (.4)ACCORDING TO THE PILOT, A LOSS OF ENGINE POWER OCCURRED, WHILE HE WAS APPLYING INSECTICIDE TO A FARM. A FORCE LANDING WAS MADE IN A PLOWED FIELD. DURING THE LANDING, THE AIRPLANE ENCOUNTERED A SMALL DITCH IN SOFT TERRAIN, AND THE AIRPLANE NOSED OVER. EXAMINATION OF THE MAINTENANCE RECORDS REVEALED THAT A TOP OVERHAUL OF THE ENGINE HAD BEEN ACCOMPLISHED, 7 DAYS BEFORE THE ACCIDENT. POSTACCIDENT EXAMINATION OF THE ENGINE REVEALED A FRACTURED CRANKSHAFT. MULTIPLE ORIGIN SITES OF THE FRACTURE WERE FOUND FROM THE SURFACE OF THE JOURNAL RADIUS. THERE WAS EVIDENCE THAT INADEQUATE TORQUE HAD BEEN APPLIED TO THE CRANKCASE THROUGH-BOLTS. THE #2 MAIN BEARING HAD MOVED FORE AND AFT IN THE BEARING BORE AND HAD ROTATED IN THE CRANKCASE; THERE WAS HEAVY FRETTING AT THE #2 AND #3 MAIN BEARING BOSS PARTING SURFACES; AND THERE WAS EVIDENCE OF SEVERE POUNDING FROM LACK OF SUPPORT THAT HAD STARTED A BREAKUP OF THE #2 BEARING. (-23) THE SPRAY PILOT WAS IN A MANEUVERING TURN WHEN THE ENGINE LOST POWER. THE PILOT MADE AN EMERGENCY LANDING IN A SOFT PLOWED FIELD. HITTING A SMALL DITCH THE PLANE FLIPPED OVER CAUSING SUBSTANTIAL DAMAGE. THE PILOT EXITED THE AIRPLANE THROUGH A SIDE WINDOW WITH NO INJURIES.
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 N53172 · 1
Matched to the same aircraft by N-number and date.