No fatalities

1994-09-14: Piper PA-60 Aerostar (Ted Smith 600) (C-FSMO) — FCF-Bowers — Saint Clair County (Port Huron), United States of America

Saint Clair County (Port Huron), United States of AmericaLanding (descent or approach)

On September 14, 1994, a Piper PA-60 Aerostar (Ted Smith 600) (registration C-FSMO) operated by FCF-Bowers was involved in an aviation accident near Saint Clair County (Port Huron), United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Inadequate preflight by the pilot resulting in fuel exhaustion. Inadequate maintenance and inspection was a factor contributing to the accident. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781208713Data APIEditorial standards

Both engines stopped near 22,000 ft; emergency landing led to tree collision. Investigation revealed fuel exhaustion due to inadequate preflight and maintenance issues with fuel cap seals.

Incident Overview

During flight, as the airplane reached an altitude of 22,000 feet, the pilot reported that both engines ceased operation within seconds of each other. While attempting an emergency landing, the aircraft struck trees. No fatalities or injuries were reported in the source.

Investigation Findings

On-scene examination found no mechanical anomalies in the engines. The fuel system was empty except for residual fuel traces in the left and right engine's fuel injector servos and flow dividers.

Fuel System Examination

Both wing fuel tank cap o-rings were hardened and exhibited flat spots. The opening tabs on the caps required forces of 8 and 3 pounds, respectively, to open. The company holding the type certificate specifies that an opening force of 16 pounds is required. The company's annual inspection checklist mandates checking these tabs, but no record of such checks was found in the airframe logbook.

Preflight and Maintenance Records

The pilot operating handbook requires that fuel cap tab tension be verified during the preflight inspection. No documentation indicated that this step was performed.

Probable Cause

The official probable cause was determined as: "Inadequate preflight by the pilot resulting in fuel exhaustion. Inadequate maintenance and inspection was a factor contributing to the accident."