De Havilland Dove

de Havilland DH.104 Dove
de Havilland Dove
Type	short-haul airliner
Manufacturer	de Havilland
Maiden flight	25 September 1945
Number built	528

The de Havilland DH.104 Dove was a British monoplane short-haul airliner from de Havilland, the successor to the biplane 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.

Contents 1 Production 2 Service 3 Variants 4 Operators 4.1 Civil operators 4.2 Military operators 5 Specifications (Dove 5) 6 External links 7 Related content

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

• Dove 1 : Light transport aircraft, seating up to 11-passengers. Powered by two 340-hp (254-kW) De Havilland Gipsy Queen 70-4 piston engines.
  • Dove 1B : Dove Mk 1 aircraft, fitted with two 380-hp (283-kW) Gipsy Queen 70-2 piston engines.
• Dove 2 : Executive transport version, seating up to six passengers. Powered by two 340-hp (254-kW) Gipsy Queen piston engines.
  • Dove 2B : Dove Mk 2 aircraft, fitted with two 380-hp (283-kW) Gipsy Queen 70-2 piston engines.
• Dove 3 : Proposed high-altitude survey version. Not built.
• Dove 4 : Military transport and communication version.
  • Devon C Mk 1 : Transport and communication version for the RAF.
  • Devon C Mk 2 : Transport and communications version for the RAF. Re-engined version of the Devon C Mk 1.
  • Sea Devon C Mk 20 : Transport and communications version for the Royal Navy.
• Dove 5 : The Dove 5 was powered by more powerful engines. The aircraft was fitted with two 380-hp (283-kW) Gipsy Queen 70-2 piston engines.
• Dove 6 : Executive transport aircraft. Uprated version of the Dove 2, powered by two 380-hp (283-kW) Gipsy Queen 70-2 piston engines.
  • Dove 6B : Stressed for operations at a maximum weight of 8,500lb (3856kg).
• Dove 7 : Uprated version of the Dove 1, fitted with two 400-hp (298-kW) Gipsy Queen 70-3 piston engines.
• Dove 8 : Uprated version of the Dove 2, fitted with two 400-hp (298-kW) Gipsy Queen 70-3 piston engines.
  • Dove 8A : Five seater version of the Dove 8 for the American market. The Dove Custom 600 was the American designation of the Dove 8A.
• Carstedt Jet Liner 600 : Conversions of the Dove, carried out by Carstedt Inc, of Long Beach, California, USA. The aircraft were fitted with two 605-ehp (451-kW) Garrett AirResearch TPE 331 turboprop engines. The fuselage was lengthened to accommodate 18 passengers.
• Riley Turbo Executive 400 : Conversions of the Dove, carried out by Riley Aircraft in the USA. The aircraft were fitted with two 400-hp (298-kW) Lycoming IO-720-A1A flat-eight piston engines.

Operators

Civil operators

•  Australia : Airlines of Western Australia
•  India : Airways (India)
• Apache Airlines
•  United Kingdom : BOAC
•  United Kingdom : British Midlands
• Cambrian
• Central African Airways
•  United Kingdom : Channel Airways
• Hunting Clan Air Transport
• Olley Air Services
• Morton Air Services
•  Belgium : SABENA
• Skyways
• South African Airways
• Sudan Airways
• Union of Burma Airways
• West African Airways
• Silver City Airways

Military operators

•  Argentina
•  Belgian Congo
•  Brazil
•  Ceylon
•  Egypt
•  Ireland: Irish Air Corps
•  Ethiopia
•  India: Indian Air Force
•  Iraq
•  Jordan
•  Lebanon
•  Malaysia
•  New Zealand: Royal New Zealand Air Force
•  Pakistan: Pakistan Air Force
•  South Africa: South African Air Force
•  Sweden
•  United Kingdom: Royal Air Force, Fleet Air Arm

Specifications (Dove 5)

Data from Jane's

General characteristics

• Crew: 2
• Capacity: 8 passengers
• Length: 39 ft 3 in (11.96 m)
• Wingspan: 57 ft (17.37 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)
• Loaded weight: 8,800 lb (4,000 kg)
• Powerplant: 2× de Havilland Gipsy Queen 70 Mk.2 geared, supercharged 6-cylinder in-line inverted air-cooled engine, 380 bhp (283 kW) each

Performance

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

External links

• Airliners.net

Related content

Related development

de Havilland Heron

Designation sequence

DH.95 Flamingo - DH.98 Mosquito - DH.100 Vampire - DH.103 Hornet - DH.104 Dove - DH.106 Comet - DH.108 Swallow

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