National Defence
Symbol of the Government of Canada
The CH-147D Chinook

Technical Specifications

Aircraft Description A twin-engine medium-to-heavy-lift helicopter acquired by the Government of Canada in 2008 from the U.S. Army under a Foreign Military Sales Agreement. Deployed with the Joint Task Force Afghanistan Air Wing in Kandahar to conduct missions that include troop movement and the transportation of equipment and supplies.
Length 30.1 m (98.7 ft)
Rotor Span 18.3 m (60 ft)
Height 5.7 m (18.7 ft)
Empty Weight 10,185 kg (22,457 lbs)
Maximum Usable Payload 12,270 kg (27,055 lbs) (external) / 33 troops (seated with equipment)
Maximum Gross Weight 22,700 kg (50,053 lbs)
Power 2 Lycoming T55-GA-714A turboshaft engines
Maximum Speed 315 km/h (196 mph) (based on outside air temperature)
Cruising Speed 220 km/h (136 mph)
Service Ceiling 5.64 km (18,504 ft)
Range 741 km (460 miles)
Equipment Hoisting systems, triple cargo-hook system, internal cargo-handling system, static-line retriever, 3 M240H 7.62 mm machine guns
Crew 1 pilot, 1 co-pilot and 2 flight engineers, plus 1 door gunner if necessary
Year(s) Procured 2008
Quantity in CF 6
Location(s) Kandahar Airfield, Afghanistan