Engine failure and propeller separation in Cessna aircraft

Casualties unknown • Aspen, CO, US

A pilot declared an emergency and performed an emergency landing after a crankshaft fracture caused the propeller and spinner to separate during climb.

What happened

While climbing at 16,000 feet, the pilot of a Cessna aircraft observed oil droplets forming on the windscreen. Following this observation, the pilot contacted air traffic control, declared an emergency, and initiated a standard rate, 180-degree turn to return to the airport.

As the turn was being completed, an audible bang and a physical shudder were felt by the pilot, after which the windscreen became covered in oil. The pilot noted a possible pitch-up motion during the event but immediately stabilized the aircraft at a best glide speed of 90 knots. Using GPS to retrace the ground track, the pilot returned to the airport, where the aircraft landed uneventfully.

The investigation

An examination of the aircraft revealed minor damage to the front of the cowling. Investigators found that the engine's crankshaft had fractured aft of the flange, and both the propeller and spinner were missing from the engine. Several months after the incident, the separated propeller assembly and crankshaft were recovered.

Detailed inspection of the engine determined that the crankshaft had fractured through at a point aft of the propeller flange. The fracture originated from a fatigue crack that began at the aft relief radius of the propeller flange.

Probable cause

A fatigue crack originating from the aft relief radius of the propeller flange caused the crankshaft to fracture, leading to the separation of the propeller assembly.

Frequently asked questions

What happened in the 2007-12-26 Piper PA-46-310P accident near Aspen, CO?

A pilot declared an emergency and performed an emergency landing after a crankshaft fracture caused the propeller and spinner to separate during climb.

What aircraft was involved and where did it happen?

The accident on 2007-12-26 involved a Piper PA-46-310P, registration N47BC, at Aspen, CO.

What was the probable cause of the accident?

A fatigue crack originating from the aft relief radius of the propeller flange caused the crankshaft to fracture, leading to the separation of the propeller assembly.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20071231X02008. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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