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De Havilland Dove

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The de Havilland DH.104 Dove was a British monoplane short-haul airliner from de Havilland, the successor to the bi-plane de Havilland Dragon Rapide and was one of Britain's most successful post-war civil designs.

The design came about from the Brabazon Committee report which called for a British designed short haul feeder for airlines.

Production

Production of the Dove and its variants consisted of 388 civilian Doves, 127 military Devon C.2s and 13 Sea Devon .

Service

The Dove first flew on 25 September 1945.

Variants

de Havilland Dove
Enlarge
de Havilland Dove

Military Operators

Specifications

General characteristics [#endnote_janes]

  • Crew: 2
  • Passengers: 8
  • Wingspan: 57 ft (17.37 m)
  • Length: 39 ft 3 in (11.96 m)
  • Height: 13 ft 4 in (4.06 m)
  • Wing area: 335 sq ft (31.1 m²)
  • Empty weight: 5,725 lb (2,600 kg)
  • Gross weight: 8,800 lb (4,000 kg)
  • Powerplant: 2x de Havilland Gipsy Queen 70 Mk 2 geared, supercharged 6-cylinder in-line inverted air-cooled engines rated at 380 bhp (283 kW).

Performance

  • Maximum speed: 202 mph (325 km/h) at 8,000 ft (2,400 m)
  • Rate of climb: 920 ft/min (4.7 m/s)
  • Service ceiling: 20,000 ft (6,100 m)
  • Maximum range: 1,070 m (1,720 km)

External links

  1. Redirect

 


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