Casualties unknown

2000-04-11: Beech B36TC (N6791P) — Fullerton, CA

Fullerton, CA, US

On April 11, 2000, a Beech B36TC (registration N6791P) was involved in an aviation accident near Fullerton, CA. Investigators recorded the probable cause as: The pilot's failure to maintain adequate airspeed while in the traffic pattern, which resulted in an inadvertent stall/spin. 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 single-engine airplane struck a house after the pilot lost control while attempting to return to the departure runway following a cabin door opening. Witnesses observed black smoke, a stall, and a spin before impact. The auxiliary fuel pump was found in the HI position.

Accident Sequence

The single-engine airplane impacted a house after experiencing a loss of control while returning to land. The commercial pilot reported to air traffic controllers that the cabin door came open during takeoff. The pilot was attempting to return the airplane to the departure runway when the air traffic controller heard the pilot's voice say, "Emergency, I've got . . ."

Witness Observations

Witnesses observed black smoke emanating from the exhaust stack. One witness observed the airplane flying low and slow at a high angle of attack with the landing gear extended. He then observed the airplane stall and spin, rotating 1.5 times before losing sight of the airplane. Another witness, who was located near the accident site, stated the engine stopped making noise prior to the accident. The airplane impacted a power line and a home in a residential area.

Post-Accident Examination

No anomalies were noted with the airplane and engine that would have prevented its operation; however, the engine did display signatures of operation with an excessively rich mixture. The auxiliary fuel pump, which was unguarded and located adjacent to the landing gear selector switch, was found in the HI position. Operation with the auxiliary fuel pump in the HI position, with an operative engine-driven fuel pump, can result in a complete loss of engine power once the pilot reduced power for landing.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X20834. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.