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General Info

De Havilland Aircraft 
DHC-2 Beaver


General information
Type STOL utility transport
National origin Canada
Manufacturer de Havilland Canada
Status Production completed
Primary users regional and remote air carriersUnited States Army
Civil Air Patrol
Number built 1,657[1]
History
Manufactured 1947–1967
Introduction date 1948
First flight 16 August 1947[1]
Developed into de Havilland Canada DHC-3 Otter
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History De Havilland Aircraft of Canada Limited (DHC)
 DHC-2 Beaver Manufactured 1947–1967



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 dusting and aerial topdressing), and civil aviation duties. Shortly after the end of the Second World War, de Havilland Canada decided to orient itself towards civilian operators. Based on feedback from pilots, the company decided that the envisioned aircraft should have excellent STOL performance, all-metal construction, and accommodate many features sought by the operators of bush planes. On 16 August 1947, the maiden flight of the aircraft, which had received the designation DHC-2 Beaver, took place. In April 1948, the first production aircraft was delivered to the Ontario Department of Lands and Forests. A Royal New Zealand Air Force (RNZAF) Beaver played a supporting role in Sir Edmund Hillary's famous 1958 Commonwealth Trans-Antarctic Expedition to the South Pole.

Development

Origins

DHC-2 on floats, operated by Kenmore Air
Instrument panel of a DHC-2 – note the single pilot's yoke, that can be handed over to the co-pilot, in flight.
Ontario Ministry of Natural Resources deHavilland DHC-2 Mk 3 Turbo Beavers on amphibious floats in Dryden, Ontario in 1995
Wipaire Boss Beaver conversion with PT6 turbine engine, retaining original fin shape and fitted with floats, at Bartow Municipal Airport, Florida in 2011

Following the end of the Second World War, de Havilland Canada's management team, recognising that there would be a corresponding downturn in military orders in the immediate post-war climate, decided to focus the company's energies upon finding work within the civilian sector. The company had recently hired Punch Dickins as Director of Sales; Dickins carried out an extensive market research program in the form of requesting and collecting feedback from other pilots, to understand what they needed in a new aircraft. It was on the basis of this information from the prospective operators themselves, as opposed to aerodynamic research or fiscal data, that the future aircraft has its origins


Design

DHC-2 MK. III Turbo Beaver

The de Havilland Canada DHC-2 Beaver is a single-engined high-wing propeller-driven STOL aircraft, principally operated as a bush plane and other utility roles, such as cargo and passenger hauling, aerial application (crop dusting and aerial topdressing), and general civil aviation purposes; aviation publication Plane & Pilot described the type as being "arguably the best bush plane ever built".[6] The Beaver was designed to operate in all seasons and the majority of weather conditions; a large proportion were also equipped with floats for buoyancy in water; it reportedly possesses favourable performance characteristics for a floatplane. As a result of its favourable characteristics as a hard working and productive aircraft, the Beaver has had a lengthy service life and many examples have been remanufactured or have otherwise received life extension modifications

 

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De Havilland Aircraft of Canada Limited (DHC) DHC-2 Beaver Manufactured 1947–1967

De Havilland Aircraft of Canada Limited (DHC)
DHC-2 Beaver Manufactured 1947–1967

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General Info

      • Cockpit crew Two pilots
        Cabin crew Two or three
        Passengers, typical 37
        Max capacity 40
        Length 73 ft (22.25 m)
        Height 24 ft 7 in (7.49 m)
        Wingspan 85 ft (25.89 m)
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Powerplant


      • Engines (2×) PW123C/D
        -100: PW120
        Unit power 2,150 hp (1,600 kW)
        -100: 1,800 hp (1,300 kW)
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Performance

  • High speed cruise 289 kn (535 km/h; 333 mph)
    -100: 270 kn (500 km/h; 310 mph)
    Ceiling 25,000 ft (7,620 m)
    Range 1,125 nmi (2,084 km; 1,295 mi)
    -100: 1,020 nmi (1,889 km; 1,174 mi)
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