17 fatalities

Quebec-Ancienne Lorette Airport Accident: Right Engine Fire and Crash (C-FQBL)

Québec-Jean Lesage (Ancienne Lorette), CanadaTakeoff (climb)

On March 29, 1979, a Fairchild F27 (registration C-FQBL) operated by Québecair was involved in an aviation accident near Québec-Jean Lesage (Ancienne Lorette), Canada during takeoff. 17 people were killed. Investigators recorded the probable cause as: The low-pressure impeller of the right (No. 2) engine burst during initial climb due to undetected fatigue cracks, causing the forward part of the engine to separate. 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 2026-06-12Data APIEditorial standards

Shortly after takeoff from Quebec-Ancienne Lorette Airport, a right engine fire forced an emergency return. The aircraft crashed in flames about 1,300 meters short of the runway, killing 17 occupants and seriously injuring seven.

Incident Overview and Immediate Sequence of Events The aircraft departed Quebec-Ancienne Lorette Airport with Montreal-Dorval Airport as its destination. Shortly after liftoff, the right engine caught fire. The captain contacted air traffic control, declared an emergency, and was cleared to return for an emergency landing. During a right turn, the aircraft lost altitude, struck the ground, and crashed in flames approximately 1,300 meters short of the runway. The accident resulted in the deaths of 17 occupants and serious injuries to seven passengers. ## Official Findings and Probable Cause The investigation determined that, during initial climb, the low-pressure impeller of the right (No. 2) engine burst, causing the forward part of the engine to separate. Engine debris damaged the electronic gear selection circuitry, preventing the landing gear from being raised. The exposed engine and lower cowl, along with the deployed gear, increased drag. In this configuration, the aircraft was unable to outclimb obstacles straight ahead or maintain altitude during the right-hand turn. Engine separation and passenger movement shifted the center of gravity beyond its aft limit. Airspeed then decreased until the aircraft struck the ground at or below the minimum control speed (Vmc). The investigation found that the low-pressure impeller burst because of fatigue cracks that had not been detected by the technicians responsible for the aircraft's maintenance.