Casualties unknown

Forced Landing After Engine Failure Results in Damage (N761RP)

Rangely, CO, US

On September 4, 1989, a Cessna T210M (registration N761RP) was involved in an aviation accident near Rangely, CO. Investigators recorded the probable cause as: Fatigue crack propagation from a subsurface flaw resulted in complete crankshaft failure. 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 2026-07-04Data APIEditorial standards

A pilot performed a forced landing with wheels up after an engine failure. The aircraft struck brush and slid 200 feet, damaging the left wing tip, engine cowling, and right wing. Postaccident analysis revealed a crankshaft failure due to a fatigue crack from a subsurface flaw.

Forced Landing

Following an engine failure, the pilot executed a forced landing onto rough and uneven terrain. Recognizing the unsuitability of the terrain for a wheels-down landing, the pilot chose to land with the landing gear retracted. Upon touchdown, the airplane struck brush and slid for 200 feet before coming to a halt.

Damage Assessment

The landing resulted in damage to the left wing tip, the engine cowling, and the right wing. No other damage to the aircraft was noted.

Engine Examination

A postaccident teardown and analysis of the engine was conducted. The examination revealed a fatigue crack that had initiated from a subsurface flaw and propagated through the material. The crankshaft had fractured between the number two and number three main bearing journals, leading to a complete crankshaft failure.

Probable cause

Fatigue crack propagation from a subsurface flaw resulted in complete crankshaft failure.

Frequently asked questions

What happened in the 4 Sept 1989 Cessna T210M accident near Rangely, CO?

A pilot performed a forced landing with wheels up after an engine failure. The aircraft struck brush and slid 200 feet, damaging the left wing tip, engine cowling, and right wing. Postaccident analysis revealed a crankshaft failure due to a fatigue crack from a subsurface flaw.

What aircraft was involved and where did it happen?

The accident on 4 Sept 1989 involved a Cessna T210M, registration N761RP, at Rangely, CO.

What was the probable cause of the accident?

Fatigue crack propagation from a subsurface flaw resulted in complete crankshaft failure.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X29346. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.