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Bristol Buckmaster

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The Bristol Buckmaster was an advanced British training aircraft operated by the Royal Air Force during the 1950s.

Design and development

By 1945, there was a serious gap in performance between the so-called advanced trainers in use – such as the Avro Anson, Airspeed Oxford, dual-control Bristol Blenheim and Lockheed Hudson – and the combat aircraft which the pilots would be expected to fly on graduation.

The Bristol response to Air Ministry Specification T.13/43 was to make further use of the Buckingham wing, with another new fuselage, in an aircraft developed as the Type 166. The trainee and instructor were seated side-by-side with a wireless operator seated behind.

The Buckmaster was a propeller-driven, twin-engine mid-wing aircraft. The retractable undercarriage was of conventional (tailwheel) configuration. The radial engines were equipped with four-blade propellers.

Operators

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Specifications

Data from Jane's Fighting Aircraft of World War II[1]

General characteristics

  • Crew: 3 (student pilot, instructor pilot, radio operator)
  • Length: 46 ft 5 in (14.2 m)
  • Wingspan: 71 ft 10 in (21.9 m)
  • Height: 17 ft 6 in (5.3 m)
  • Wing area: 708 ft² (65.8 m²)
  • Empty weight: 24,042 lb (10,900 kg)
  • Loaded weight: 33,700 lb (15,280 kg)
  • Powerplant:Bristol Centaurus VII 18-cylinder radial engines, 2,585 hp (1,880 kW) each

Performance


See also

Related development

Comparable aircraft

Related lists

References

  1. Jane, Fred T. “The Bristol 166 Buckmaster.” Jane’s Fighting Aircraft of World War II. London: Studio, 1946. p. 113. ISBN 1 85170 493 0.

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This article is licensed under the GNU Free Documentation License.
It uses material from the Wikipedia article "Bristol Buckmaster".