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Last updated: 20 November 2017
Fecha:domingo 16 junio 1996
Tipo:Silhouette image of generic DHC3 model; specific model in this crash may look slightly different
de Havilland Canada DHC-3 Otter
Operador:Wildcountry Airways
Registración: C-FMEL
Numéro de série: 222
Año de Construcción: 1957
Motores: 1 Pratt & Whitney R-1340
Tripulación:Fatalidades: 0 / Ocupantes: 1
Pasajeros:Fatalidades: 0 / Ocupantes: 6
Total:Fatalidades: 0 / Ocupantes: 7
Daños en la Aeronave: Anulado
Consecuencias: Written off (damaged beyond repair)
Ubicación:9 km (5.6 milles) E of Cochenour, ON (   Canadá)
Fase: Desconocido (UNK)
Naturaleza:Vuelo Doméstico No Programado
Aeropuerto de Salida:Cochenour, ON, Canadá
Aeropuerto de Llegada:Sandy Beach Lodge, ON, Canadá
The pilot had levelled the aircraft and configured it for cruise flight at approximately 2,500 feet above sea level when the pilot heard a popping sound and noted a slight loss of engine power, and wisps of whitish-grey smoke entered the cabin. The aircraft instruments indicated normal engine operation, and the fire warning system did not activate. The pilot suspected that the engine had suffered a cylinder failure and turned to return to Cochenour. A passenger seated in the right front crew
seat reported flames near the floor at the front, right corner of the cockpit. The pilot radioed the Thunder Bay Flight Service Station to advise of
the emergency, had the passenger vacate the crew seat, and attempted to suppress the fire with a hand-held extinguisher. Thick, black smoke billowed
into the cabin, restricting visibility and causing respiratory distress for all of the occupants. The pilot opened the left crew door in order to see
ahead and landed the aircraft, still on fire, on McNeely Bay, the first available landing site. The aircraft landed hard but remained upright on the
floats. The occupants left by the main door, with their life jackets, and were picked up almost immediately by nearby boats. The aircraft was consumed
by fire within minutes after landing.

Probable Cause:

CAUSES AND CONTRIBUTING FACTORS: "Continued operation of the engine following an exhaust valve failure on the No. 2 cylinder resulted in a flaming gas path near the right side of the firewall, an exhaust system overheat, and a subsequent cabin fire."

Accident investigation:
Investigating agency: TSB Canada
Status: Investigation completed
Duration: 1 year and 1 months
Accident number: TSB Report A96C0091
Download report: Final report


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This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
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