Casualties unknown

1999-02-12: Cessna 210G (N5874F) — Red Baron Aviation — Lake Placid, FL

Lake Placid, FL, US

On February 12, 1999, a Cessna 210G (registration N5874F) operated by Red Baron Aviation was involved in an aviation accident near Lake Placid, FL. Investigators recorded the probable cause as: Crankshaft fatigue crack originating from the aft fillet radius of the No. 2 main journal. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 1 related events involving the same aircraft type or operator are linked below.

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

A pilot heard a snap/thud and popping noise, followed by engine stoppage. After an unsuccessful airborne restart, the pilot landed in a pasture. The airplane struck a tree and a gully, separating the left wing and landing gear. Investigation revealed a crankshaft fatigue crack from a shifted bearing.

Flight Details

The purpose of the flight was to position the airplane at Miami's Opa Locka Airport. While at an altitude of 5,000 feet agl under radar control, the pilot heard a 'snap/thud, followed by a popping noise.' This was followed by an engine and propeller stoppage. An airborne restart was unsuccessful, and the propeller would not turn.

Forced Landing

Realizing he could not make it safely to an airport, the pilot landed the airplane in a pasture. During the landing, the airplane struck a tree, separating the left wing from the airframe. Additionally, the nose and right main landing gear collided with a gully, causing them to separate.

Investigation Findings

According to the operator's records, the engine was remanufactured by Continental Motors on December 9, 1997, and had 1622.9 hours of operating time since installation. The crankshaft was examined at the NTSB Materials Laboratory. The examination revealed that the crankshaft separated due to a fatigue crack that originated from the aft fillet radius of the No. 2 main journal. The fatigue area contained circumferential gouge marks and heat damage that were consistent with a bearing shell that had rotated or shifted. The bearing shell from the No. 1 rod journal also contained wear damage on the aft and forward edges that were consistent with shifting during engine operation.

Probable cause

Crankshaft fatigue crack originating from the aft fillet radius of the No. 2 main journal

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001205X00211. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.