Training flight accident near RAF Fairford

6 fatalities • Fairford AFB, United Kingdom • Takeoff (climb)

A training mission departing from RAF Fairford resulted in a fatal crash after an engine shutdown procedure led to unintended reverse thrust.

What happened

During a scheduled training flight operating out of RAF Fairford, the crew was performing specific engine management procedures. As the aircraft began its initial climb, the captain instructed the co-pilot, who was performing the task under supervision, to shut down the number four engine and feather the propeller.

During this process, an error occurred when the co-pilot accidentally engaged the reverse thrust system. This action created a significant imbalance in power between the engines, known as asymmetric thrust. The resulting loss of control caused the aircraft to descend into an open field, where it impacted the ground and caught fire. There were six fatalities among the occupants of the aircraft.

Findings

  • The accident was triggered by the unintentional activation of the reverse thrust system during an engine shutdown maneuver.
  • The sequence of events began during the initial climb phase of the flight.

Probable cause

The accidental engagement of the reverse thrust mechanism during an engine shutdown procedure caused asymmetric thrust and subsequent loss of control.

Frequently asked questions

What happened in the 1969-03-24 Lockheed C-130 Hercules accident near Fairford AFB, United Kingdom?

A training mission departing from RAF Fairford resulted in a fatal crash after an engine shutdown procedure led to unintended reverse thrust.

Were there any fatalities in the 1969-03-24 Lockheed C-130 Hercules accident?

The accident was fatal, resulting in 6 fatalities.

What aircraft was involved and where did it happen?

The accident on 1969-03-24 involved a Lockheed C-130 Hercules, registration XV180, operated by Royal Air Force - RAF, at Fairford AFB, United Kingdom.

What was the probable cause of the accident?

The accidental engagement of the reverse thrust mechanism during an engine shutdown procedure caused asymmetric thrust and subsequent loss of control.

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