4 fatalities

Fatal Crash of Training Aircraft Near Toronto After Wing Failure (55-3252)

Toronto-Downsview, CanadaFlight

On February 14, 1956, a De Havilland DHC-3 Otter (registration 55-3252) operated by United States Army was involved in an aviation accident near Toronto-Downsview, Canada in flight. 4 people were killed. Investigators recorded the probable cause as: The failure of the right wing was caused by excessive negative lift forces upon the aircraft, resulting in complete severance. This force was imposed by penetration of the wing vortex turbulence area caused by a Avro Canada CF-100 Canuck. 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)Source recordUpdated 2026-07-04Data APIEditorial standards

A single-engine airplane on a local training flight from Toronto-Downsview Airport crashed after its right wing detached due to excessive negative lift forces from a CF-100 Canuck's wake turbulence. All four occupants were killed.

Accident Summary

On a local training flight from Toronto-Downsview Airport, a single-engine airplane crashed approximately 17 minutes after takeoff. The aircraft was cruising near the airfield when its right wing suffered a structural failure, detaching from the fuselage. The separated wing passed over the fuselage and struck the tail, shearing it off. The airplane then dove out of control into a snow-covered field and burst into flames upon impact, resulting in its total destruction. All four occupants were killed.

Aircraft and Crew

The aircraft was carrying one Canadian instructor from De Havilland and three pilots from the US Army, including one pilot and two student pilots. The crew consisted of William A. Ferderber (instructor), Major Aaron G. Atkisson (student pilot), Captain James P. Dowling (student pilot), and Captain Louis Durant (pilot).

Probable Cause

The official investigation determined that the right wing failure was caused by excessive negative lift forces imposed on the aircraft, leading to complete severance. These forces resulted from the aircraft penetrating the wing vortex turbulence area of an Avro Canada CF-100 Canuck, generating negative G forces beyond the design criteria of the airplane.

Frequently asked questions

What happened in the 14 Feb 1956 De Havilland DHC-3 Otter accident near Toronto-Downsview, Canada?

A single-engine airplane on a local training flight from Toronto-Downsview Airport crashed after its right wing detached due to excessive negative lift forces from a CF-100 Canuck's wake turbulence. All four occupants were killed.

Were there any fatalities in the 14 Feb 1956 De Havilland DHC-3 Otter accident?

The accident was fatal, resulting in 4 fatalities.

What aircraft was involved and where did it happen?

The accident on 14 Feb 1956 involved a De Havilland DHC-3 Otter, registration 55-3252, operated by United States Army, at Toronto-Downsview, Canada.

What was the probable cause of the accident?

The failure of the right wing was caused by excessive negative lift forces upon the aircraft, resulting in complete severance. This force was imposed by penetration of the wing vortex turbulence area caused by a Avro Canada CF-100 Canuck. These negative G forces were in excess of the design criteria for the aircraft.