ASN logo
Accident description
Last updated: 19 October 2017
Status:Final
Date:Friday 26 September 2014
Time:17:40
Type:Silhouette image of generic BE10 model; specific model in this crash may look slightly different
Beechcraft A100 King Air
Operator:Air Creebec
Registration: C-FEYT
C/n / msn: B-210
First flight: 1975
Total airframe hrs:14985
Cycles:15570
Crew:Fatalities: 0 / Occupants: 2
Passengers:Fatalities: 0 / Occupants: 7
Total:Fatalities: 0 / Occupants: 9
Airplane damage: Substantial
Airplane fate: Written off (damaged beyond repair)
Location:Timmins Airport, ON (YTS) (   Canada)
Phase: Landing (LDG)
Nature:Domestic Scheduled Passenger
Departure airport:Moosonee Airport, ON (YMO/CYMO), Canada
Destination airport:Timmins Airport, ON (YTS/CYTS), Canada
Flightnumber: 140
Narrative:
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
Add your photo of this accident or aircraft
 

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.
languages: languages

Share