No fatalities

Fuel Exhaustion Results in Dual Engine Power Loss and Forced Landing (N10AS)

Detroit, United States of AmericaFlight

On November 19, 1987, a Volpar Turboliner 18 (registration N10AS) operated by Connie Kalitta Services was involved in an aviation accident near Detroit, United States of America in flight. No fatalities were reported. Investigators recorded the probable cause as: Fuel exhaustion (nonmechanical) due to incorrect fuel quantity gage readings, pilot inattentiveness, and poor planning/decision making. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

A pilot experienced total loss of engine power in both engines due to fuel exhaustion while en route. Forced landing resulted in collision with a tree and rocky berm, causing landing gear collapse.

Incident Overview

While returning to home base after delivering revenue cargo, the pilot encountered a total loss of engine power in both engines. The cause was determined to be fuel exhaustion. In response, the pilot executed emergency procedures and prepared for a forced landing.

Forced Landing and Impact

The aircraft was directed toward a grassy field bordering a lake. During the landing, the aircraft first struck a tree and then the rocky berm of the shoreline. The impact with the berm caused the landing gear to detach. The aircraft then swerved and slid backwards before coming to rest approximately 150 feet from the lake's edge.

Post-Accident Findings

A post-accident investigation revealed that each wing tank contained less than 2 gallons of fuel. The official probable cause identified fuel exhaustion as the reason for the nonmechanical loss of engine power. Contributing factors included incorrect fuel quantity gauge indications, pilot inattentiveness, and poor planning and decision-making by the pilot.

Sequence of Events

  • Occurrence #1: Loss of engine power (total, nonmechanical) during descent due to fuel exhaustion.
  • Occurrence #2: Forced landing initiated during descent phase.
  • Occurrence #3: In-flight collision with terrain (tree and berm) during the forced landing, resulting in landing gear collapse and aircraft damage.