deHavilland CC-108A CARIBOU

The DeHavilland-built Caribou transport aircraft was designed with Short Take-Off and Landing (STOL) characteristics. It featured a conventional stressed skin construction and had a cantilever -wing with full-span double-slotted flaps with the outer portions acting as ailerons. It was the first DeHavilland Canada aircraft to feature a retractable undercarriage.

The RCAF initially selected the Caribou to fulfill UN support duties for the Congo purchasing four aircraft along with a range of support equipment. The aircraft were never deployed to the Congo but did see action in an extensive range of UN missions. The Caribou also proved popular with other armed forces such as the United States Army and the Royal Australian and Malaysian Air Forces. The Caribou has seen extensive use as a light tactical transport in a variety of military and now civilian uses.

aircraft specifications
CDN Reg: CC-108A
US/NATO Reg.: C-7A
Manufacturer: DeHavilland Canada : designed and built
Crew / Passengers: 2 pilots, 1 flt engineer & 30 passengers or 32 troops
Power Plant(s): two 1,450 ESHP Pratt & Whitney R2000-7M2 Twin Wasp piston engines
Performance: Maximum Speed: 214 mph (344 km/h) Cruising Speed: 180 mph (290 km/h) Service Ceiling: 27,500 ft (8,381 m)
Weights: Empty: 17,630 lb (12,247 kg) Gross: 28,500 lb (22,317 kg)
Dimensions: Span: 95 ft 7 1/2 in (29.15 m) Length: 72 ft 7 in (22.12 m) Height: 31 ft 9 in (9.67 m) Wing Area: 912 sq ft (84.7 sq m)
Armament: None
RCAF deHavilland CC-108 Caribou

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