Aircraft loss during post-maintenance test flight at Goose Bay

3 fatalities • Goose Bay, Canada • Takeoff (climb)

A structural failure occurred during a climb following takeoff from Goose Bay Airport, resulting in the deaths of all three crew members.

What happened

During a scheduled check flight following maintenance work, an aircraft was performing a climb shortly after departing Goose Bay Airport. Approximately two minutes into the flight, the crew attempted to extend the flaps. During this maneuver, the aircraft experienced a stall and the left wing separated from its root. The loss of structural integrity caused the plane to enter an uncontrollable dive, impacting the ground. There were three fatalities among the crew, which consisted of two pilots and one mechanic.

Findings

Investigations into the accident determined that the primary factor was a sudden and unplanned full retraction of the flaps. This event caused the nose of the aircraft to pitch downward abruptly. The resulting aerodynamic loads placed on the wing exceeded its structural design limits, leading to the separation of the left wing. The detached wing subsequently struck the tail section, making the crash inevitable.

Probable cause

The sudden, spontaneous retraction of the flaps created excessive structural loads that caused the left wing to fail.

Frequently asked questions

What happened in the 1956-04-10 De Havilland DHC-3 Otter accident near Goose Bay, Canada?

A structural failure occurred during a climb following takeoff from Goose Bay Airport, resulting in the deaths of all three crew members.

Were there any fatalities in the 1956-04-10 De Havilland DHC-3 Otter accident?

The accident was fatal, resulting in 3 fatalities.

What aircraft was involved and where did it happen?

The accident on 1956-04-10 involved a De Havilland DHC-3 Otter, registration 3666, operated by Royal Canadian Air Force - RCAF, at Goose Bay, Canada.

What was the probable cause of the accident?

The sudden, spontaneous retraction of the flaps created excessive structural loads that caused the left wing to fail.

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