No fatalities

1999-05-29: Piper PA-60 Aerostar (Ted Smith 600) (N601JS) — Alpha Beta Aviation — Montgomery, United States of America

Montgomery, United States of AmericaTakeoff (climb)

On May 29, 1999, a Piper PA-60 Aerostar (Ted Smith 600) (registration N601JS) operated by Alpha Beta Aviation was involved in an aviation accident near Montgomery, United States of America during takeoff. No fatalities were reported. Investigators recorded the probable cause as: The pilot's inadvertent shutdown of the wrong engine that resulted in the total loss of engine power. A factor was the loss of engine power due to fuel starvation when the left fuel boost pump failed. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781204344Data APIEditorial standards

During takeoff, the left engine lost power. After the pilot feathered the left propeller, the right engine also lost power, forcing a landing. Examination revealed the right mixture lever was in the lean position and the left fuel boost pump had failed.

Accident Summary

During the takeoff roll and initial climb, both engines were producing normal power. As the airplane climbed through 150 feet, the left engine lost power. The pilot reported that he feathered the left propeller. Following the securing of the left engine, the right engine began to 'power down.' The pilot reported that he was unable to maintain a climb attitude and was forced to land on the airport in a grassy area.

Examination Findings

The subsequent examination of the cockpit disclosed that the left engine throttle was in the full forward position, and the right throttle lever was in the mid-range position. Both propeller levers were found full forward. The left engine mixture lever was in the full forward position, and the right mixture lever full aft, or lean, position.

A functional check of both engines was conducted. Initially the left engine would not start, but after troubleshooting the fuel system, the left fuel boost pump was determined to have been defective.

Probable Cause

The official probable cause is the pilot's inadvertent shutdown of the wrong engine that resulted in the total loss of engine power. A factor was the loss of engine power due to fuel starvation when the left fuel boost pump failed.