De Havilland Canada DHC-3 Otter
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- The correct title of this article is de Havilland Canada DHC-3 Otter. The initial letter is shown capitalized due to technical restrictions.
| DHC-3 Otter | |
|---|---|
| Turbo Otter in Harbour Air livery | |
| Type | STOL utility transport |
| Manufacturer | de Havilland Canada |
Another in de Havilland Canada's successful line of rugged and useful STOL utility transports, the single engined, high wing, propeller-driven DHC-3 Otter was conceived to be capable of performing the same roles as the earlier and highly successful Beaver, but was bigger, the vertible "one-ton truck."
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[edit] Design and development
de Havilland Canada began design work on the King Beaver(the Otter's original name) in January, 1951, with Canadian certification given in November, 1952. Using the same overall configuration of the earlier and highly successful DHC2 Beaver, the new design incorporated a longer fuselage, greater span wings and is much heavier. Seating in the main cabin is for 10 or 11, whereas the Beaver could seat six. Power is supplied by a 450kW (600hp) Pratt & Whitney R1340 Wasp radial. Like the Beaver, the Otter can be fitted with skis and floats. The amphibious floatplane Otter features a unique four unit retractable undercarriage, with the wheels retracting into the floats. The Otter served as the basis for the very successful Twin Otter which featured two wing mounted Pratt and Whitney PT-6 turboprops.
[edit] Operational use
Although the Otter found ready acceptance in bush airlines, as in a similar scenario to the DHC-2 Beaver, the US Army soon became the largest operator of the aircraft (184 delivered with the designation U-1A Otter). Other military users included Australia, Canada and India but the primary role of the aircraft as a rugged bush plane continues to this day.
[edit] Military operators
- Argentina, Australia, Bangladesh, Burma, Cambodia, Canada, Chile, Colombia, Costa Rica, Ethiopia, Ghana, India, Indonesia, New Zealand, Nicaragua, Nigeria, Norway, Panama, Paraguay, Philippines, United Kingdom , United States (US Army, US Navy).
[edit] Turbo Otter
Some aircraft were converted to turbine power using a Pratt & Whitney Canada PT6A turboprop. The Walter 601 Turboprop engine, manufactured in the Czech Republic, may also be fitted to the Otter. The PZL radial engine from the Antonov An-2, a plane that fulfills a very similar role, may also be fitted to the Otter.
[edit] Specifications
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General characteristics<h3>
- Crew: 1
- Length: 41 ft in (12.5 m)
- Wingspan: 58 ft in (17.7 m)
- Height: 13 ft in (4 m)
- Wing area: ft² (m²)
- Empty weight: 5287 lb (2398 kg)
- Loaded weight: 8000 lb (3628 kg)
- Useful load: lb (kg)
- Max takeoff weight: lb (kg)
- Powerplant: 1× Pratt & Whitney S1H1-g Wasp radial , 600 hp (447 kW)
<h3>Performance<h3>
- Never exceed speed: knots (mph, km/h)
- Maximum speed: knots (160 mph, 258 km/h)
- Cruise speed: knots (mph, km/h)
- Stall speed: knots (mph, km/h)
- Range: nm (960 mi, 1545 km)
- Service ceiling: 17900 ft (5460 m)
- Rate of climb: 1000 ft/min (305 m/min)
- Wing loading: lb/ft² (kg/m²)
- Power/mass: hp/lb (W/kg)
[edit] Reference
- Hotson, Fred W. The de Havilland Canada Story. Toronto: CANAV Books, 1983. ISBN 0-07-549483-3.
[edit] See also
[edit] Related content
Related development<h3>
<h3>Comparable aircraft<h3> <h3>Designation sequence<h3> DHC-1 - DHC-2 - DHC-3 - DHC-4 - DHC-5 - DHC-6<h3>See also<h3>
Gipsy Moth • Tiger Moth • Fox Moth • Mosquito • DHC-1 Chipmunk • DHC-2 Beaver • DHC-3 Otter • DHC-4 Caribou • DHC-5 Buffalo • DHC-6 Twin Otter • DHC-7 Dash 7 • DHC-8 Dash 8


