2 fatalities

1983-06-22: Douglas C-47 Skytrain (DC-3) (C-GUBT) — Skycraft Air Transport — Toronto-Lester Bowles Pearson, Canada

Toronto-Lester Bowles Pearson, CanadaLanding (descent or approach)

On June 22, 1983, a Douglas C-47 Skytrain (DC-3) (registration C-GUBT) operated by Skycraft Air Transport was involved in an aviation accident near Toronto-Lester Bowles Pearson, Canada during landing or approach. 2 people were killed. Investigators recorded the probable cause as: The aircraft's weight and centre of gravity limits were exceeded, and the cargo was not secured. These factors led to loss of control of the aircraft. 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 1781220378Data APIEditorial standards
Aircraft registered C-GUBT
Aircraft registered C-GUBT. Photo: Ian Gratton / CC BY 2.0, via Wikimedia Commons

Skycraft Air Transport Flight 505, a Douglas C-47A, crashed while on final approach to Toronto International Airport after losing control due to weight and center of gravity exceedances and unsecured cargo. Both pilots were killed.

Accident Overview

On a cargo flight from Cleveland-Hopkins International Airport to Toronto International Airport, a Douglas C-47A aircraft operated by Skycraft Air Transport as Flight 505 was destroyed when it crashed during final approach. Both pilots sustained fatal injuries. The flight carried six wire mesh baskets nearly filled with automobile roof bows. Before departure, the crew chief asked if the load should be tied down; the pilots responded that they would handle it.

Flight and Approach

Flight 505 departed Cleveland at 07:45 under visual flight rules. Upon nearing Toronto, the terminal controller provided heading adjustments to align the aircraft with the instrument landing system localizer for an almost straight-in approach to Runway 06R. The flight was then transferred to the arrival controller, who continued vectoring. During the approach, the arrival controller twice instructed Flight 505 to maintain best speed for spacing from other traffic. The crew initially reported they were flying at maximum speed, and later indicated they were at best speed because the aircraft was fairly heavy. The flight called the tower after passing the outer marker and received clearance to land.

Loss of Control

After crossing the runway threshold at an altitude of 100 to 150 feet, the aircraft's nose smoothly rose by 5 to 10 degrees, then dropped by a similar amount as if correcting the nose-high attitude. This pitch up and down motion was quickly followed by two pitch oscillations of increasing speed and magnitude. On the fourth oscillation, the nose continued to rise to 45 to 60 degrees, and the aircraft began to climb. Engine noise seemed to increase as the aircraft pitched up for the last time. At approximately 200 feet, at the apex of the climb, the left wing dropped and the aircraft yawed left about 90 degrees. The wings then leveled, and the aircraft fell into a field to the right of the runway. The time from the first oscillation to impact was estimated at about 10 seconds.

Post-Impact Fire

Upon impact, the right main landing gear ruptured a fuel tank, leading to a post-impact fuel fire that consumed the aircraft.

Probable Cause

The official investigation determined the probable cause to be that the aircraft's weight and center of gravity limits were exceeded, and the cargo was not secured. These factors led to a loss of control.