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Percival Provost

Military Aircraft

The Percival P.56 Provost was a single-engined basic trainer that replaced the Prentice in Royal Air Force service in the 1950s. Designed in response to Air Ministry specification T.16/48, it was an all-metal low-wing monoplane with fixed landing gear and side-by-side seating, so that an instructor could sit beside the student and watch and demonstrate directly. The first prototype flew on 24 February 1950, and the production Provost T.1 used a 550 horsepower Alvis Leonides radial engine, roughly twice the power of the Prentice. The RAF placed its first order for 200 aircraft in 1951, production ended in 1961 after about 461 had been built, and armed and unarmed versions were exported to air forces including Ireland, Iraq, Burma, Sudan, Rhodesia and Oman. A turbojet development became the Jet Provost.

Facts
Year
1950 1
Engine Class
Piston 1
Status
Out of production 1
Power (kW)
410 1
Units Built
461 1
Top Speed (km/h)
322 1
Mass (kg)
1520 1
Engine
Alvis Leonides 126 1
Comparison
Body Style
Aircraft (no road body style) 1
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Exemplifies

Aviation, Modes
Source Percival Provost (Wikipedia)

Of Make

Source Percival Provost (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Percival Provost (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
designed and manufactured by British aviation company Percival

Originated In

Also in Geography Atlas: where this subject originated.

Source Percival Provost (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
designed and manufactured by British aviation company Percival
Sources
1. Percival Provost (Wikipedia)
  • Development, first flight
    First flying on 24 February 1950
  • Lead
    single-engined low-wing monoplane
  • Specifications, powerplant
    Alvis Leonides 126 9-cylinder air-cooled radial piston engine, 550 hp (410 kW)
  • Specifications, engine type
    Alvis Leonides 126 9-cylinder air-cooled radial piston engine
  • Specifications, engine power
    550 hp (410 kW)
  • Specifications, empty weight
    Empty weight: 3,350 lb (1,520 kg)
  • Specifications, performance
    Maximum speed: 200 mph (320 km/h, 170 kn) at sea level
  • Development, production total
    a total of 461 aircraft had reportedly been completed
  • Development, end of production
    During 1961, production of the type was terminated
  • Lead, manufacturer
    designed and manufactured by British aviation company Percival
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