2 fatalities

Left Wing Failure During Training Flight Leads to Crash of DC-3C at Pickle Lake (C-FADD)

Pickle Lake, CanadaLanding (descent or approach)

On May 11, 1987, a Douglas C-47 Skytrain (DC-3) (registration C-FADD) operated by Northland Air Manitoba was involved in an aviation accident near Pickle Lake, Canada during landing or approach. 2 people were killed. Investigators recorded the probable cause as: It was determined that the left wing failed under normal flight loads as a result of a fatigue crack in the centre section lower wing skin. Anomalies in the radiographs taken during mandatory non-destructive testing inspections were not correctly interpreted. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 2 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

A Douglas DC-3C experienced a left wing failure during a training flight near Pickle Lake, Ontario, after a fatigue crack in the lower wing skin went undetected in radiographic inspections.

Flight Details

The aircraft, a Douglas DC-3C registered as C-FADD, was returning to Pickle Lake from Big Trout Lake after delivering a cargo of fuel. This was the third and final operation of the day. Prior to landing, the pilot informed the company dispatch office of an intention to conduct local training for the co-pilot, who was scheduled for an upgrade to captain status the following month. The captain, a company training pilot, occupied the right seat.

Sequence of Events

The aircraft entered a west-to-east holding pattern at the airport's Non-Directional Beacon (NDB), descending in stages from 8,500 feet above sea level (asl) to 2,700 feet asl, which was the appropriate altitude for an instrument approach. The pilot transmitted that they would execute an NDB approach and subsequently reported during the procedure turn inbound to the airfield. About three minutes later, two other pilots flying in the vicinity observed the aircraft in a descent with the left wing folded upward. The aircraft continued descending in an inverted attitude until it struck the ground.

Investigation Findings

The investigation determined that the left wing failed under normal flight loads as a result of a fatigue crack in the centre section lower wing skin. Anomalies in the radiographs taken during mandatory non-destructive testing inspections were not correctly interpreted.

Probable cause

It was determined that the left wing failed under normal flight loads as a result of a fatigue crack in the centre section lower wing skin. Anomalies in the radiographs taken during mandatory non-destructive testing inspections were not correctly interpreted.