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De Havilland Canada DHC-3 Otter

General Aviation and Light Aircraft

The DHC-3 Otter is a single-engined, high-wing, propeller-driven short take-off and landing aircraft developed by de Havilland Canada as a larger, more powerful companion to its Beaver. Conceived in January 1951 and nicknamed the King Beaver during design, it was meant to be the one-ton truck to the Beaver's half-ton. It kept the Beaver's layout but added a longer fuselage, a wing of greater span and a cruciform tail, and its cabin seated ten or eleven instead of six. A Pratt & Whitney R-1340 geared radial of 600 horsepower drove it. The Otter was certified in Canada in November 1952 and entered production soon afterward, and 466 were built. Like the Beaver it can be fitted with skis or floats, and it served as the basis for the twin-engined Twin Otter.

Facts
Year
1952 1
Engine Class
Piston 1
Units Built
466 1
Top Speed (km/h)
260 1
Mass (kg)
1863 1
Maximum Mass (kg)
3629 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source De Havilland Canada DHC-3 Otter (Wikipedia)

Of Make

Source De Havilland Canada DHC-3 Otter (Wikipedia)
Sources
1. De Havilland Canada DHC-3 Otter (Wikipedia)
  • Design and development, certification
    The Otter received Canadian certification in November 1952 and entered production shortly thereafter.
  • Lead
    single-engined, high-wing, propeller-driven, short take-off and landing (STOL) aircraft
  • Specifications
    air-cooled radial piston engine
  • Specifications, empty weight
    Empty weight: 4,108 lb (1,863 kg)
  • Specifications, gross weight
    Gross weight: 8,000 lb (3,629 kg)
  • Specifications, maximum speed
    Maximum speed: 160 mph (260 km/h, 140 kn) at 5,000 ft (1,524 m)
  • Design and development, production
    A total of 466 Otters were manufactured.
  • Lead, manufacturer
    developed by de Havilland Canada
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