Casualties unknown

Boeing 737-217 Engine Failure During Landing in Fredericton

Fredericton, New Brunswick, CA

On November 13, 2000, a Boeing 737-217, C-GKCP operated by Canadian Airlines International was involved in an aviation accident near Fredericton, New Brunswick, CA. Investigators recorded the probable cause as: A single 4th-stage turbine wheel blade failed as a result of an extension of a fatigue crack propagating through the chord from the trailing edge, precipitating the overload failure of the remaining 4th-stage blades. This summary draws on records from the Transportation Safety Board of Canada (TSB); 5 related events involving the same aircraft type or operator are linked below.

Sourcesthe Transportation Safety Board of Canada (TSB)Primary reportUpdated 2026-09-13Data APIEditorial standards
Boeing 737-217, C-GKCP
Photo: San Diego Air & Space Museum Archives / Public domain, via Wikimedia Commons

A Boeing 737-217 experienced a No. 1 engine failure during landing in Fredericton, New Brunswick, after a 4th-stage low-pressure turbine blade failed due to fatigue. The aircraft landed safely, and the failure was contained.

Incident Overview and Immediate Response On a flight from Québec, Quebec, a Boeing 737-217 was landing on runway 15 in Fredericton, New Brunswick. During the landing roll, the No. 1 engine, a Pratt & Whitney JT8D-17A, spooled down after the thrust reversers were deployed, and flames were observed from the tail pipe. The crew secured the engine and brought the aircraft to a stop on the runway. A flight service station specialist observed flames on the left side of the aircraft and advised the crew, who requested further assistance. The crash alarm was activated, and airport firefighters arrived at the scene in approximately 1 minute and 10 seconds. Following a visual inspection by airport firefighters, the aircraft taxied to the ramp, where passengers and crew deplaned normally.

Probable cause

A single 4th-stage turbine wheel blade failed as a result of an extension of a fatigue crack propagating through the chord from the trailing edge, precipitating the overload failure of the remaining 4th-stage blades.