Casualties unknown

2005-12-12: Beech A23 (N3590R) — Mammoth Lakes, CA

Mammoth Lakes, CA, US

On December 12, 2005, a Beech A23 (registration N3590R) was involved in an aviation accident near Mammoth Lakes, CA. Investigators recorded the probable cause as: a loss of engine power for undetermined reasons, and, the failure of the pilot to maintain an adequate airspeed while maneuvering following the loss of power, which resulted in a 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

An airplane collided with flat desert terrain after an in-flight loss of control. Witnesses reported a rough-running engine, popping sounds, and a subsequent tumble. No mechanical discrepancies were found in the engine teardown.

Accident Overview

The airplane impacted flat desert terrain following an in-flight loss of control. A witness located about 1 mile south of the accident site heard a rough running engine and looked up to identify the source. As the aircraft passed overhead, the witness reported hearing the engine popping and backfiring for approximately 3 seconds, after which the engine stopped operating.

Witness Observations

The witness then observed the airplane dip to the right in a tumbling motion, describing it as a somersault with the nose dropping and the tail coming over the top. The aircraft completed about 2 to 3 revolutions over a duration of roughly 8 seconds before descending below tree level and colliding with the ground. The witness noted that it was somewhat cloudy in the area, but the airplane was below the clouds. Upon reaching the accident site to render assistance, the witness reported no frost or ice on the wings and stated that the ambient temperature was not cold enough for frost or ice formation.

Additional witnesses at the departure airport reported that the engine sounded as though the exhaust system was leaking severely, or that the exhaust or muffler was loose.

Engine Examination

An engine test run could not be performed due to displacement of the crankshaft caused by the nose-down impact. However, a subsequent engine teardown revealed no discrepancies in the engine core or its accessories that would have precluded normal operation.

Investigation Findings

The investigation did not establish a definitive cause for the engine roughness or failure. No evidence of pre-existing mechanical issues was found in the engine components. The witness descriptions indicate an in-flight loss of control following the engine stoppage, leading to the collision with terrain.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20051223X02007. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.