de Havilland DH.50

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DH.50
A DH.50J of Qantas.
Role Transport biplane
Manufacturer de Havilland
First flight 30 July 1923
Introduction 1923
Retired 1942
Primary users Qantas
Imperial Airways
Number built 38

The de Havilland DH.50 was a 1920s British large single-engined biplane transport built by de Havilland at Stag Lane Aerodrome, Edgware, and licence-built in Australia, Belgium, and Czechoslovakia.

History

In the early 1920s,

engine
fits.

In 1924, Cobham won the

Pacific Islands.[1]

Licence production

The aircraft was popular in Australia and de Havilland licensed its production there, leading to 16 aircraft being built.

Royal Flying Doctor Service of Australia
.

Variants

  • DH.50 : Single-engined light transport biplane.
DH.50A Bell Bird (G-AUEK)
  • DH.50A : Powered by one 240 hp (179 kW) Siddeley Puma inline engine.
  • DH.50J : The Australian-built Qantas fleet were powered by one 450 hp (287 kW) Bristol Jupiter Mk IV radial engine. Other radial engines were fitted in other aircraft in the DH50J series.[5]

Operators

Australia
  • Australian Aerial Services Ltd
  • Holdens Air Transport
Qantas DH.50J Atalanta (VH-UHE)
Belgium
Czechoslovakia
Iraq
  • Iraq Petroleum Transport Company Ltd
New Zealand
United Kingdom
  • Air Taxis Ltd
  • Brooklands School of Flying Ltd
  • Imperial Airways Ltd
  • North Sea Aerial and General Transport Company Ltd
  • Northern Air Lines Ltd

Specifications (DH.50 with Puma engine)

Data from De Havilland Aircraft since 1909[6]

General characteristics

  • Crew: 1
  • Capacity: 4 passengers
  • Length: 29 ft 9 in (9.07 m)
  • Wingspan: 42 ft 9 in (13.03 m)
  • Height: 11 ft 0 in (3.35 m)
  • Wing area: 434 sq ft (40.3 m2)
  • Empty weight: 2,413 lb (1,095 kg)
  • Gross weight: 4,200 lb (1,905 kg)
  • Powerplant: 1 × Siddeley Puma 6-cylinder water-cooled in-line piston engine, 230 hp (170 kW)
  • Propellers: 2-bladed fixed-pitch propeller

Performance

  • Maximum speed: 109 mph (175 km/h, 95 kn)
  • Cruise speed: 95 mph (153 km/h, 83 kn)
  • Range: 380 mi (610 km, 330 nmi)
  • Service ceiling: 14,600 ft (4,500 m)
  • Rate of climb: 605 ft/min (3.07 m/s)
  • Wing loading: 8.99 lb/sq ft (43.9 kg/m2)
  • Power/mass: 0.059 hp/lb (0.097 kW/kg)

See also

Related lists

References

Notes

  1. ^ Stephens 2006, pp. 39–41.
  2. ^ a b Wilson 1994, p. 216
  3. ^ Stroud 1988, p. 43.
  4. ^ Crook 1997, p. 21.
  5. ^ Gunn 1985[page needed]
  6. ^ Jackson 1987, p. 190

Bibliography

External links