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The de Havilland Canada DHC-2 Beaver is a single-engined high-wing propeller-driven short takeoff and landing (STOL) aircraft developed and manufactured by de Havilland Canada. It has been primarily operated as a bush plane and has been used for a wide variety of utility roles, such as cargo and passenger hauling, aerial application ( crop ...
de Havilland Canada or Viking Air DHC-2 Beaver: Bush plane: One crew and 7 passengers 1947 1947–1967 1,657 de Havilland Canada DHC-3 Otter: STOL bush plane One crew and up to 11 passengers 1951 1953–1967 466 Grumman/de Havilland Canada CS2F Tracker: Anti-submarine warfare for the Royal Canadian Navy: Four crew 1956 1956 42 CS2F-1 57 CS2F-2
The de Havilland Canada DHC-3 Otter is a single-engined, high-wing, propeller-driven, short take-off and landing aircraft developed by de Havilland Canada. It was conceived to be capable of performing the same roles as the earlier and highly successful Beaver , including as a bush plane , but is overall a larger aircraft.
In May 2005, the company subsequently purchased the parts and service business for all the older de Havilland Canada aircraft from Bombardier Aerospace. [8] On 24 February 2006, Viking purchased the type certificates from Bombardier for all the discontinued de Havilland Canada designs: the DHC-1 Chipmunk, DHC-2 Beaver, DHC-3 Otter, DHC-4 Caribou, DHC-5 Buffalo, DHC-6 Twin Otter and DHC-7 Dash ...
De Havilland Canada DHC-2 Beaver This page was last edited on 27 December 2022, at 23:21 (UTC). Text is available under the Creative Commons Attribution ...
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Data from Jane's All the World's Aircraft 1984-85 General characteristics Crew: 1 Capacity: 7 pax Length: 24 ft 0 in (7.32 m) Wingspan: 30 ft 3 in (9.22 m) Width: 9 ft (2.7 m) folded Height: 9 ft 7 in (2.92 m) Wing area: 159.3 sq ft (14.80 m 2) Aspect ratio: 5.7 Airfoil: NACA 4415 Empty weight: 2,050 lb (930 kg) Max takeoff weight: 3,800 lb (1,724 kg) MTOW and MLW Fuel capacity: 56 US gal (47 ...
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