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Last updated: 12 December 2019
Statuts:Enquête Officielle
Date:vendredi 26 septembre 2014
Heure:17:40
Type/Sous-type:Silhouette image of generic BE10 model; specific model in this crash may look slightly different
Beechcraft A100 King Air
Compagnie:Air Creebec
Immatriculation: C-FEYT
Numéro de série: B-210
Année de Fabrication: 1975
Heures de vol:14985
Cycles:15570
Equipage:victimes: 0 / à bord: 2
Passagers:victimes: 0 / à bord: 7
Total:victimes: 0 / à bord: 9
Dégats de l'appareil: Substantiels
Conséquences: Written off (damaged beyond repair)
Lieu de l'accident:Timmins Airport, ON (YTS) (   Canada)
Phase de vol: A l'atterrissage (LDG)
Nature:Transport de Passagers Nat.
Aéroport de départ:Moosonee Airport, ON (YMO/CYMO), Canada
Aéroport de destination:Timmins Airport, ON (YTS/CYTS), Canada
Numéro de vol:YN140
Détails:
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


Photos

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

Plan
Ce plan montre l'aéroport de départ ainsi que la supposée destination du vol. La ligne fixe reliant les deux aéroports n'est pas le plan de vol exact.
La distance entre Moosonee Airport, ON et Timmins Airport, ON est de 305 km (191 miles).

Les informations ci-dessus ne représentent pas l'opinion de la 'Flight Safety Foundation' ou de 'Aviation Safety Network' sur les causes de l'accident. Ces informations prélimimaires sont basées sur les faits tel qu'ils sont connus à ce jour.
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