Casualties unknown

2002-03-30: Mooney M20F (N9530M) — Grapeland, TX

Grapeland, TX, US

On March 30, 2002, a Mooney M20F (registration N9530M) was involved in an aviation accident near Grapeland, TX. Investigators recorded the probable cause as: The loss of engine power due to the #2 connecting rod cap separating from the connecting rod. A contributing factor was the limited forward visibility due to oil on the windscreen. 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

During cruise flight, a sudden vibration and oil-covered windscreen prompted a forced landing. The aircraft touched down with gear retracted, bounced, and struck a cattle feeder before coming to rest. Engine examination revealed a detached connecting rod and case damage.

Incident

Approximately 25 minutes after departure, while in cruise flight at 1,500 feet mean sea level, a sudden vibration shook the airplane. The pilot scanned the engine instruments and noted that everything "appeared to be normal." Subsequently, oil covered the windscreen, severely limiting forward visibility. The pilot initiated a forced landing to a grass field with the landing gear in the retracted position. During the landing, the airplane bounced, and the left wing "skimmed" across the top of a metal cattle feeder before impacting the ground. The airplane then spun around approximately 450 degrees and came to rest upright.

Examination

Examination of the engine revealed two holes on the top and bottom of the engine case between the #1 and #2 cylinders. The #2 connecting rod was found sticking out of the top hole and was not attached to the crankshaft. The #2 connecting rod cap was found separated from the connecting rod. The #2 connecting rod cap attachment bolts, nut, and both bearings were missing and not located. The other attachment bolt was found lodged inside the crankcase next to the #3 cylinder opening. The camshaft exhibited impact damage and was fractured in half at the point where the #2 connecting rod was found positioned.

Maintenance History

Review of the maintenance records revealed the engine had accumulated 997.75 hours since major overhaul at the time of the last annual inspection. Further review indicated that the last entry in the engine logbook was an oil change, with 1097.4 hours since major overhaul.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020402X00448. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.