129 fatalities

1953-06-18: Douglas C-124 Globemaster II (51-0137) — United States Air Force - USAF (since 1947) — Tachikawa AFB (Tokyo), Japan

Tachikawa AFB (Tokyo), JapanLanding (descent or approach)

On June 18, 1953, a Douglas C-124 Globemaster II (registration 51-0137) operated by United States Air Force - USAF (since 1947) was involved in an aviation accident near Tachikawa AFB (Tokyo), Japan during landing or approach. 129 people were killed. Investigators recorded the probable cause as: The aircraft stalled due to improper approach configuration and low airspeed following an engine failure. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781253198Data APIEditorial standards

A military transport aircraft carrying 129 people crashed short of the runway during an emergency landing attempt following an engine failure.

What happened

During a flight returning to Seoul, a military transport aircraft was transporting 122 soldiers on leave along with a crew of seven. Shortly after departing, as the plane reached an altitude of approximately 1,000 feet, the pilot notified air traffic control that the third engine had failed. Following this notification, the crew was authorized to perform an emergency return to the airfield.

While executing the circuit for landing, the pilot requested additional power and deployed the flaps to their full extent. During this final approach, the aircraft type experienced a stall, leading to a crash in a field located 5.6 km before reaching the runway. The impact resulted in a massive explosion, and a subsequent fire burned through the wreckage for several hours. There were 129 fatalities among the occupants, with no survivors recorded.

Findings

Investigations into the accident identified that the third engine failed shortly after takeoff for reasons that remained undetermined. The primary factor leading to the crash was an aerodynamic stall caused by a combination of insufficient approach speed and an incorrect configuration involving fully extended flaps during the final phase of flight.

Probable cause

The aircraft stalled due to improper approach configuration and low airspeed following an engine failure.