Casualties unknown

1997-09-26: Cessna P210N (N6394W) — Creswell, OR

Creswell, OR, US

On September 26, 1997, a Cessna P210N (registration N6394W) was involved in an aviation accident near Creswell, OR. Investigators recorded the probable cause as: The pilot's improper fuel management in which the fuel selector was positioned on tank with inadequate fuel resulting in fuel starvation. Also causal was the pilot's failure to perform the pilot operating handbook 'engine failure in flight' procedure. 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

A pilot reported moving the fuel selector from 'both' to 'right' after takeoff and not repositioning it, leading to fuel starvation. The aircraft made an emergency forced landing, striking a ditch and flipping over. Post-accident examination confirmed 35 gallons of fuel in the left tank and the selector on 'right'.

Event Summary

A pilot reported that shortly after takeoff, the fuel selector was moved from the 'both' position to the 'right' position and was not subsequently repositioned. This resulted in fuel starvation as the aircraft cruised at 16,000 feet about three hours after takeoff.

Emergency Response

The pilot declared an emergency with air traffic control (ATC) and was directed to a nearby airport. The pilot attempted a forced landing but was not successful in reaching the runway. During the landing, the airplane struck a ditch and flipped over, coming to rest in a field near the runway.

Post-Accident Examination

Post-accident examination revealed 35 gallons of fuel in the left tank, no fuel in the right tank, and the fuel selector positioned to 'right.'

Performance and Procedures

According to the pilot's operating handbook (POH), the airplane takes approximately 15 minutes to descend from 16,000 feet to the emergency airport elevation of 535 feet above mean sea level. This descent is at best glide speed (approximately 85 knots indicated airspeed) with the propeller windmilling and flaps and gear up. The POH 'engine failure in flight' procedure directs the pilot to check fuel quantity and place the fuel selector on the fullest tank.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X08938. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.