5 fatalities

1959-11-04: Douglas C-54 Skymaster (CF-ILI) — Wheeler Airlines — Saint-Cléophas-de-Brandon, Canada

Saint-Cléophas-de-Brandon, CanadaFlight

On November 4, 1959, a Douglas C-54 Skymaster (registration CF-ILI) operated by Wheeler Airlines was involved in an aviation accident near Saint-Cléophas-de-Brandon, Canada in flight. 5 people were killed. Investigators recorded the probable cause as: An engine fire of unknown origin became uncontrollable and led to the structural failure of the left wing during an emergency descent. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 6 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781247082Data APIEditorial standards

A cargo flight operating from Montreal-Dorval experienced an engine fire and subsequent mid-air structural failure, resulting in the loss of all five crew members.

What happened

On a scheduled cargo flight from Montreal-Dorval to Hall Beach, Northwest Territories, a DC-4 departed runway 10 at 22:44 local time. After departing, the aircraft maintained its runway heading and ascended to 6,000 feet before turning toward its assigned course and climbing further to 9,000 feet. By 22:59, the aircraft had reached its target altitude.

Shortly after reaching this level, the crew initiated an emergency descent due to a fire in the number two engine. During the descent, the final radio transmission occurred at 23:07, during which the crew reported that the left wing had separated from the aircraft and that the plane was in a spin. The DC-4 disintegrated while in flight, leaving debris scattered across an area measuring approximately 1.25 by 0.75 miles. There were five fatalities among the crew members.

Findings

Investigations determined that an unidentified fire began within the number two engine nacelle during the climb. The fire grew to a magnitude that exceeded the capacity of the onboard extinguishing systems. Several contributing factors were identified, including:

  • The degraded state of the exhaust collector ring.
  • Potential deterioration of flexible wire braid hose assemblies.
  • The likely application of high power settings during the ascent.
  • A possible failure in the fire detection and warning system to alert the crew before the fire breached the firewall and ignited the fuel feed and oil tank.

During the rapid descent, structural stresses caused by maneuvers or atmospheric gusts were sufficient to sever the left wing spar.

Probable cause

An engine fire of unknown origin became uncontrollable and led to the structural failure of the left wing during an emergency descent.