6 fatalities

1991-06-30: Beechcraft 65 Queen Air (N713JB) — Richard E. Stahl — Pioneer, United States of America

Pioneer, United States of AmericaFlight

On June 30, 1991, a Beechcraft 65 Queen Air (registration N713JB) operated by Richard E. Stahl was involved in an aviation accident near Pioneer, United States of America in flight. 6 people were killed. Investigators recorded the probable cause as: Improper emergency procedures by the pilot, when he inadvertently shut down the left engine after encountering a partial loss of power in the right engine. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781211884Data APIEditorial standards

A Beech 65 crashed into trees following a loss of control in flight. The right engine had a broken exhaust valve; the left propeller was feathered. All six occupants were killed.

Accident Details

A Beech 65 aircraft collided with trees in mountainous terrain after an inflight loss of control. A witness observed the airplane initiate a right turn, then roll to the right until inverted and enter a spin. The aircraft was in a steep nose-down attitude when it began to pull out. A ground witness heard the engines, initially mistaking the sound for an approaching motorcycle.

The pilot had initially flown the aircraft 45 days before the accident, logging 3.5 hours of dual instruction. No record of additional flight training was found in the pilot's logbook after that date. The pilot satisfactorily completed a check flight in a Cessna 150 four days before the accident.

Investigation Findings

Examination of the wreckage revealed that the right engine had a broken exhaust valve, while the left propeller was feathered. No preexisting mechanical malfunctions or failures were found with the left engine. The aircraft was destroyed in the accident.

Probable Cause

The official probable cause of the accident was improper emergency procedures by the pilot, who inadvertently shut down the left engine after encountering a partial loss of power in the right engine. Factors related to the accident were: improper installation of the right engine's #6 exhaust valve seat by other maintenance personnel, fatigue failure of the #6 exhaust valve, and the pilot's lack of familiarity with the aircraft.