de Havilland DH.50
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 : 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
- Rockhampton Aerial Services Ltd
- Royal Australian Air Force[2]
- West Australian Airlines Ltd
- 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
- List of aircraft of the Royal Australian Air Force
- List of aircraft of the Royal New Zealand Air Force and Royal New Zealand Navy
References
Notes
- ^ Stephens 2006, pp. 39–41.
- ^ a b Wilson 1994, p. 216
- ^ Stroud 1988, p. 43.
- ^ Crook 1997, p. 21.
- ^ Gunn 1985[page needed]
- ^ Jackson 1987, p. 190
Bibliography
- The Illustrated Encyclopedia of Aircraft. Orbis Publishing. (part work 1982–85)
- Crook, John (1997). Air Transport the First Fifty Years. The Archive Photographs Series. Stroud: Chalford. p. 21. ISBN 0-7524-0790-2.
- Grant, James Ritchie. "Anti-Clockwise: Australia the Wrong Way". Air Enthusiast, No. 82, July–August 1999, pp. 60–63. ISSN 0143-5450
- Gunn, John (1985). The Defeat of Distance: Qantas 1919–1939. Brisbane: University of Queensland Press. ISBN 978-0702217074.
- Jackson, A. J. (1973). British Civil Aircraft since 1919. Vol. 2. London: Putnam. ISBN 0-370-10010-7.
- Jackson, A. J. (1987). De Havilland Aircraft since 1909 (Second ed.). London: Putnam. ISBN 0-85177-802-X.
- Kucera, Pavel (August 1990). "Czech fifties — Part 1". ISSN 0143-7240.
- Kucera, Pavel (September 1990). "Czech fifties — Part 2". Aeroplane Monthly. Vol. 18, no. 9. pp. 551–553. ISSN 0143-7240.
- Prins, François (Spring 1994). "Pioneering Spirit: The QANTAS Story". ISSN 0143-5450.
- Stephens, Alan (2006) [2001]. The Royal Australian Air Force: A History. London: Oxford University Press. pp. 39–41. ISBN 0-19-555541-4.
- Stroud, John (January 1988). "Wings of Peace". Aeroplane Monthly. Vol. 16, no. 1. pp. 41–46. ISSN 0143-7240.
- Wilson, Stewart (1994). Military Aircraft of Australia. Weston Creek: Aerospace Publications. p. 216. ISBN 1875671080.
- "A New De Havilland Commercial Aeroplane". Flight. Vol. XV, no. 32. 9 August 1923. pp. 473–477. Retrieved 6 January 2024.
External links
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