Casualties unknown

2004-10-27: Cessna T210N (N6108Y) — Raymond, MS

Raymond, MS, US

On October 27, 2004, a Cessna T210N (registration N6108Y) was involved in an aviation accident near Raymond, MS. Investigators recorded the probable cause as: The total loss of engine power which was initiated by fretting of the crankcase halves for undetermined reasons, causing rotation of several of the main bearings, oil starvation, and subsequent failure of several of the connecting rods. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

After takeoff, the pilot heard a loud bang and felt shaking; smoke filled the cockpit. The engine failed, and the pilot performed a forced landing in a field, landing hard and nosing over before the aircraft caught fire. The pilot exited through the window. Engine examination revealed main bearing shifting and connecting rod failures.

Accident Sequence

After takeoff, the flight climbed to 6,000 feet. As the pilot leveled off, he heard a "loud bang" and felt the airframe shaking. The cockpit then filled with smoke, and he requested a vector to the nearest airport. He attempted to keep the engine running but was unsuccessful. The flight descended and broke out of the clouds at 200 feet above ground level, where he slowed the airplane to less than the best glide airspeed to clear power lines. The airplane landed "rather hard" in a field against furrows, nosed over, then burst into flames. The pilot exited the airplane from the pilot's window.

Engine Examination

Examination of the engine revealed fretting at the main bearing support faying surfaces, with resulting shifting of the No. 2 main bearing. Lubrication distress was noted at all main bearing and connecting rod journals, and for Nos. 3-6 connecting rod bearings. The Nos. 1 and 2 connecting rods were fractured, while one of the connecting rod bolts for the No. 3 cylinder was fractured with necking present. The engine was last overhauled on October 1, 2002, and installed in the accident airplane on October 28, 2002. The engine had accumulated 1,297 hours since being overhauled at the time of the failure, and there was no record that any cylinders had been removed or replaced since the overhaul.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20041101X01730. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.