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Last updated: 15 November 2019
Estado:Final
Fecha:viernes 26 septiembre 2014
Hora:17:40
Tipo:Silhouette image of generic BE10 model; specific model in this crash may look slightly different
Beechcraft A100 King Air
Operador:Air Creebec
Registración: C-FEYT
Numéro de série: B-210
Año de Construcción: 1975
Horas Totales de la Célula:14985
Ciclos:15570
Tripulación:Fatalidades: 0 / Ocupantes: 2
Pasajeros:Fatalidades: 0 / Ocupantes: 7
Total:Fatalidades: 0 / Ocupantes: 9
Daños en la Aeronave: Considerable
Consecuencias: Written off (damaged beyond repair)
Ubicación:Timmins Airport, ON (YTS) (   Canadá)
Fase: Aterrizaje (LDG)
Naturaleza:Vuelo Doméstico Programado
Aeropuerto de Salida:Moosonee Airport, ON (YMO/CYMO), Canadá
Aeropuerto de Llegada:Timmins Airport, ON (YTS/CYTS), Canadá
Número de Vuelo:YN140
Descripción:
The Air Creebec Beechcraft King Air A100 aircraft (registration C-FEYT, serial number B-210) was operating as Air Creebec flight 140 on a scheduled flight from Moosonee, Ontario, to Timmins, Ontario, with 2 crew members and 7 passengers on board. While on approach to Timmins, the crew selected landing gear down, but did not get an indication in the handle that the landing gear was down and locked. A fly-by at the airport provided visual confirmation that the landing gear was not fully extended. The crew followed the Quick Reference Handbook procedures and selected the alternate landing-gear extension system, but they were unable to lower the landing gear manually. An emergency was declared, and the aircraft landed with only the nose gear partially extended. The aircraft came to rest beyond the end of Runway 28. All occupants evacuated the aircraft through the main entrance door. No fire occurred, and there were no injuries to the occupants. Emergency services were on scene for the evacuation.

Probable Cause:

Findings as to causes and contributing factors:
1. During the extension of the landing gear, a wire bundle became entangled around the landing-gear rotating torque shaft, preventing full extension of the landing gear.
2. The entanglement by the wire bundle also prevented the alternate landing-gear extension system from working. The crew was required to conduct a landing with only the nose gear partially extended.

Other findings
1. The wire bundle consisted of wiring for the generator control circuits, and when damaged, disabled both generators. The battery became the only source of electrical power until the aircraft landed.

Accident investigation:
cover
Investigating agency: TSB Canada
Status: Investigation completed
Duration: 1 year and 4 months
Accident number: A14O0178
Download report: Final report


Fotos

photo of Beechcraft-A100-King-Air-C-FEYT
accident date: 26-09-2014
type: Beechcraft A100 King Air
registration: C-FEYT
 

Map
This map shows the airport of departure and the intended destination of the flight. The line between the airports does not display the exact flight path.
Distance from Moosonee Airport, ON to Timmins Airport, ON as the crow flies is 305 km (191 miles).

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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