Armstrong Whitworth Argosy

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Argosy
Type airliner
Manufacturer Armstrong Whitworth
Maiden flight March 1926
Primary user Imperial Airways
Number built 7


For the 1950s transport, see Armstrong Whitworth AW.660 Argosy

The Armstrong Whitworth Argosy was a British three-engined biplane airliner built by Armstrong Whitworth Aircraft and operated by Imperial Airways from 1926 to 1935.

Contents

The Armstrong Whitworth Argosy stemmed from a declaration by Imperial Airways that all its aircraft would be multi-engined designs on the grounds of safety [1]. They were intended to replace the older single-engined de Havilland aircraft that Imperial Airways had inherited from its constituent companies, mainly Daimler Airways. The first example (G-ELBF ) flew in March 1926 [2] following an initial order for three Argosies from Imperial Airways.

The Argosy was initially used on European routes (later operating on services to South Africa), with the fleet named after famous cities. Argosies implemented the world's first "named" air service, the luxury 'Silver Wing' service from London to Paris[3], in Argosy City of Birmingham (G-EBLO). Two seats were removed and replaced with a bar and a steward was in attendance.

Three Argosies were lost during service with Imperial Airways, with one being written off in a forced landing near Aswan and one during a training accident, both in 1931, with no-one being hurt in either accident. In March 1933, however, an Argosy caught fire over Belgium , causing a crash in which all 3 crew and 12 passengers were killed [1].

Argosies continued in service with Imperial Airways until 1935, with the last example being used for joy-riding by United Airways Ltd of Blackpool airport, which then became British Airways Ltd. It continued in use with British Airways until December 1936.

  • Argosy Mk I : Three engined airliner. Powered by three 385 hp (287 kW) Armstrong Siddeley Jaguar IIIA radial piston engines. Later fitted with Jaguar IVA engines. Three constructed.
  • Argosy Mk II : Three engined airliner. Powered by three 420 hp (313 kW) Armstrong Siddeley Jaguar IVA radial piston engines. Four constructed.

Data from {British Civil Aircraft since 1919}[1]

General characteristics

  • Crew: 2
  • Capacity: 20
  • Length: 64 ft 6 in (19.66 m)
  • Wingspan: 90 ft (27.44 m)
  • Height: 19 ft (5.79 m)
  • Wing area: 1,890 ft² (176 m²)
  • Empty weight: 12,090 lb (5,495 kg)
  • Max takeoff weight: 19,200 lb (8,727 kg)
  • Powerplant:Armstrong Siddeley Jaguar IVA Radial, 420 hp (313 kW) each

Performance

  1. ^ a b c Jackson, A.J (1973). British Civil Aircraft since 1919 Volume 1., 2nd Edition, Putnam & Co. ISBN 0-370-10006-9. 
  2. ^ (1997) in David Donald: The Encyclopedia of World Aircraft. Aerospace Publishing. ISBN 1-85605-375-X. 
  3. ^ (1980) in M J H Taylor: Jane's Encyclopedia of Aircraft. Jane's Publishing Company. 
  • (1980) in M J H Taylor: Jane's Encyclopedia of Aircraft. Jane's Publishing Company. 


 

 

 

 

 


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