15 fatalities

1956-08-29: Douglas DC-6 (CF-CUP) — Canadian Pacific Airlines - CP Air — Cold Bay (ex Fort Randall AAF & Thornbrough AFB), United States of America

Cold Bay (ex Fort Randall AAF & Thornbrough AFB), United States of AmericaLanding (descent or approach)

On August 29, 1956, a Douglas DC-6 (registration CF-CUP) operated by Canadian Pacific Airlines - CP Air was involved in an aviation accident near Cold Bay (ex Fort Randall AAF & Thornbrough AFB), United States of America during landing or approach. 15 people were killed. Investigators recorded the probable cause as: The crew failed to take corrective action after the wing flaps were fully retracted during a low-altitude circling approach. 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 1781250028Data APIEditorial standards

A scheduled flight from Vancouver to Hong Kong crashed during a circling approach at Cold Bay, resulting in 15 fatalities.

What happened

On the scheduled route from Vancouver, British Columbia, to Hong Kong via Cold Bay and Tokyo, Flight 307 was operating with a crew of 8 and 14 passengers. At approximately 20:35 Bering standard time, the aircraft was positioned over the outbound range station at Cold Bay, performing a standard instrument approach. The flight completed a procedure turn by 20:42.

During the final stages of the approach, the aircraft type (unspecified) was seen descending through overcast conditions toward runway 14. After crossing the airfield at a low altitude, the aircraft began a shallow left turn toward the intersection of the two runways before disappearing from view to the southeast. A fire was subsequently identified, and it was confirmed that the plane had crashed. The accident resulted in 15 fatalities, consisting of 11 passengers and 4 crew members. The impact and subsequent fire caused the total destruction of the aircraft.

Findings

Investigation into the crash determined that the full retraction of the wing flaps at a low altitude during a circling approach was the primary factor in the accident. Evidence suggests that the crew did not take the required corrective measures following this configuration change. While a circling approach typically requires flaps to be extended 20 degrees, the flaps were found in a fully retracted state. This loss of lift likely prevented the aircraft from maintaining sufficient altitude during the turn, as very little altitude was gained after power was applied.

Probable cause

The crew failed to take corrective action after the wing flaps were fully retracted during a low-altitude circling approach.