19960211047439A

Accident · No damage

FAA accident report · Cessna 172K · Hedley, TX · February 11, 1996

Date
February 11, 1996 · 17:30 local
Place
Hedley, TX
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N7358G
NTSB investigation
NTSBFTW96LA116
Reported as
Cessna 172K

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-16) This accident was the result of an engine that failed mechanically in flight resulting in a forced landing in a soft field that flipped the aircraft over causing substantial damage. The engine in this aircraft had been recently overhauled by a local mechanic that failed to properly torque the connecting rod bolts, which resulted in a catastrophic failure. Failure to properly torque the connecting rod bolts is contrary to CFR 14 part 43.13(a). Further, the mechanic that performed the overhaul did not comply with airworthiness directive 91-14-22 on the crankshaft gear that was applicable and due at the time of the overhaul.

As the FAA filed it

(-16) THIS ACCIDENT WAS THE RESULT OF AN ENGINE THAT FAILED MECHANICALLY IN FLIGHT RESULTING IN A FORCED LANDING IN A SOFT FIELD THAT FLIPPED THE AIRCRAFT OVER CAUSING SUBSTANTIAL DAMAGE. THE ENGINE IN THIS AIRCRAFT HAD BEEN RECENTLY OVERHAULED BY A LOCAL MECHANIC THAT FAILED TO PROPERLY TORQUE THE CONNECTING ROD BOLTS, WHICH RESULTED IN A CATASTROPHIC FAILURE. FAILURE TO PROPERLY TORQUE THE CONNECTING ROD BOLTS IS CONTRARY TO CFR 14 PART 43.13(A). FURTHER, THE MECHANIC THAT PERFORMED THE OVERHAUL DID NOT COMPLY WITH AIRWORTHINESS DIRECTIVE 91-14-22 ON THE CRANKSHAFT GEAR THAT WAS APPLICABLE AND DUE AT THE TIME OF THE OVERHAUL.

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 N7358G · 1

Matched to the same aircraft by N-number and date.