1 fatality

1990-11-29: Piper PA-31 Cheyenne (N1879W) — Century Life of America — Des Moines, United States of America

Des Moines, United States of AmericaLanding (descent or approach)

On November 29, 1990, a Piper PA-31 Cheyenne (registration N1879W) operated by Century Life of America was involved in an aviation accident near Des Moines, United States of America during landing or approach. One person was killed. Investigators recorded the probable cause as: The pilot's improper emergency procedures by not feathering the left engine after it lost power and/or was shut down, and his failure to keep the aircraft at or above the minimum control airspeed (VMC), which resulted in a loss of aircraft control. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781212405Data APIEditorial standards

On final approach, a pilot reported possible engine shutdown, then the aircraft rolled left and descended into terrain. Investigation found left engine not developing power, propeller not feathered.

Incident Overview

During the final approach to landing, after receiving clearance to land, the pilot informed the air traffic controller that he might need to shut down an engine. The pilot declined to declare an emergency or request assistance. On short final, the aircraft was observed to roll to the left and descend into the terrain.

Examination Findings

Subsequent examination of the wreckage revealed evidence that the left engine was not developing power at the time of impact, although the left propeller was not feathered. Evidence also indicated that the right engine was producing high power during the impact. No mechanical deficiency of the left engine or propeller was found.

Pilot and Occupants

The pilot, who was the sole occupant on board, was killed in the accident.

Probable Cause

According to the official investigation, the probable cause of the accident was the pilot's improper emergency procedures by not feathering the left engine after it lost power and/or was shut down, and his failure to keep the aircraft at or above the minimum control airspeed (VMC), which resulted in a loss of aircraft control. An additional factor was an undetermined problem concerning the left engine that caused it to lose power or prompted the pilot to shut it down.