3 fatalities

Engine No. 2 Thrust Reversal Leads to Fatal Crash After Aborted Takeoff (N280F)

Saint Louis-Lambert, United States of AmericaTakeoff (climb)

On July 6, 1977, a Lockheed L-188 Electra (registration N280F) operated by Fleming International Airways was involved in an aviation accident near Saint Louis-Lambert, United States of America during takeoff. 3 people were killed. Investigators recorded the probable cause as: Uncontrolled descent during initial climb due to unwanted thrust reversal on engine number two. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-12Data APIEditorial standards

Aircraft crashed during second takeoff after first was aborted due to propeller autofeather. Uncontrolled descent caused by unwanted thrust reversal on engine No. 2. Three crew killed.

Event Overview

The accident involved an aircraft that experienced a takeoff abort followed by a fatal crash on a subsequent takeoff attempt. The airplane was destroyed and all three crew members were killed.

First Takeoff Abort

During the initial takeoff procedure, the propeller on engine number two autofeathered, prompting the crew to abandon the takeoff.

Second Takeoff and Crash

The crew initiated a second takeoff. While in the initial climb phase, the aircraft entered an uncontrolled descent and crashed in flames near the runway. All three occupants were killed.

Probable Cause

The official probable cause was determined to be an uncontrolled descent during initial climb due to unwanted thrust reversal on engine number two.

Contributing Factors

Several contributing factors were identified:

  • The pilot-in-command exercised poor judgment.
  • Attempted operation with known deficiencies in equipment.
  • Failed to follow approved procedures.
  • Unwanted thrust reversal occurred.
  • Oil exhaustion in the propeller system.
  • Propeller system feathering pump leakage.
  • Inadequate maintenance and inspection.
  • Deficiency in company-maintained equipment, services, and regulation.
  • Pilot fatigue.
  • Improper oil replacement.
  • Bad pump output O-rings.