de Havilland DH.51

The de Havilland DH.51 is a 1920s British three-seat touring biplane built by de Havilland at Stag Lane Aerodrome, Edgware.

DH.51
Airworthy DH.51, G-EBIR, at the Shuttleworth Collection
Role Touring biplane
Manufacturer de Havilland
First flight 1924
Number built 3

Design and development

De Havilland designed the DH.51 as an economical touring biplane, based on the 90 hp (67 kW) RAF 1A engine which was available from war-surplus stocks. The aircraft first flew in July 1924; it performed well but because it did not have a dual-ignition system it was refused a certificate of airworthiness. As it would have taken at least ten hours of flight testing to certify it with a single-ignition system, de Havilland decided to re-engine the aircraft instead. The aircraft was fitted with an ADC Airdisco Air-cooled V8 piston engine, which considerably improved performance but was no longer cheap to operate. As a result, only three aircraft were built. The first aircraft was fitted with single-bay wings and was designated the DH.51A. It was exported to Australia and later converted to a floatplane as the DH.51B.

Operational service

The first aircraft was exported to Australia in 1927, as a floatplane it capsized in Sydney Harbour in January 1931. The second aircraft was used in Britain until it was scrapped in 1933. The third aircraft was exported to Kenya in 1929. It returned to Britain in 1965 and is still in use today.

Surviving aircraft

The third aircraft built (registered G-EBIR and named Miss Kenya; built in 1925) is still airworthy and on public display at the Shuttleworth Collection, Old Warden, England.

Specifications (DH.51 Airdisco engine)

Data from De Havilland Aircraft since 1909[1]

General characteristics

  • Crew: 1
  • Capacity: 2 passengers
  • Length: 26 ft 6 in (8.08 m)
  • Wingspan: 37 ft 0 in (11.28 m)
  • Height: 9 ft 9 in (2.97 m)
  • Wing area: 325 sq ft (30.2 m2)
  • Empty weight: 1,342 lb (609 kg)
  • Gross weight: 2,240 lb (1,016 kg)
  • Powerplant: 1 × ADC Airdisco V-8 air-cooled piston engine, 120 hp (89 kW)
  • Propellers: 4-bladed fixed-pitch

Performance

  • Maximum speed: 108 mph (174 km/h, 94 kn)
  • Stall speed: 43 mph (69 km/h, 37 kn)
  • Service ceiling: 15,000 ft (4,600 m)
  • Rate of climb: 960 ft/min (4.9 m/s)

See also

References
  1. Jackson 1987, p. 199.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985). Orbis Publishing.
  • Jackson, A.J. (1973). British Civil Aircraft since 1919 Volume 2. London: Putnam. ISBN 0-370-10010-7.
  • Jackson, A.J. (1987). De Havilland Aircraft since 1909 (Third ed.). London: Putnam. ISBN 0-85177-802-X.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.