Boulton Paul P.71A

The Boulton & Paul P.71A was a 1930s British twin-engined all-metal biplane transport aircraft developed by Boulton & Paul Ltd from the unsuccessful P.64 Mailplane to meet an Imperial Airways requirement for a mail plane.

P.71A
Boulton-Paul P.71A G-ACOX Boadicea
Role Mail plane/Light Transport
Manufacturer Boulton & Paul Ltd
Introduction 1935
Retired 1936
Status Destroyed
Primary user Imperial Airways
Number built 2
Developed from Boulton Paul P.64 Mailplane

History

The P.71A was the successor to the Boulton & Paul's first attempt to meet the airline requirement, the P.64 Mailplane. The P.71A was lighter, slimmer and longer and used Armstrong Siddeley Jaguar IVA radial piston engines.

Two aircraft were built and delivered to Imperial Airways at Croydon Airport in February 1935. The airline had lost interest in using them as mailplanes, so the two aircraft were converted as VIP transports with 13 removable seats.

G-ACOX

The first aircraft, registered G-ACOX and named Boadicea after the Briton queen of that name, was lost in the English Channel on 25 September 1936 while on an air-mail flight from Croydon to Paris with the loss of the two crew.

G-ACOY

The second aircraft, registered G-ACOY and named Britomart after the literary character of that name, was damaged beyond repair in a landing accident at Haren, Brussels on 25 October 1935.

Operators

 United Kingdom

Specifications

Boulton Paul P.71A 3-view drawing from NACA-AC-199

Data from Imperial Airway's Latest [1]

General characteristics

  • Crew: 2
  • Capacity: 6–7 passengers[2]
  • Length: 44 ft 2 in (13.46 m)
  • Wingspan: 54 ft 0 in (16.46 m)
  • Height: 15 ft 2 14 in (4.629 m)
  • Wing area: 718.5 sq ft (66.75 m2)
  • Aspect ratio: 7.91:1
  • Empty weight: 6,100 lb (2,767 kg)
  • Gross weight: 9,500 lb (4,309 kg)
  • Fuel capacity: 186 imp gal (223 US gal; 850 L)
  • Powerplant: 2 × Armstrong Siddeley Jaguar VIA 14-cylinder radial engines, 490 hp (370 kW) each

Performance

  • Maximum speed: 195 mph (314 km/h, 169 kn) [3]
  • Cruise speed: 150 mph (240 km/h, 130 kn) at 4,500 ft (1,400 m)
  • Range: 600 mi (970 km, 520 nmi) (full tanks)
  • Service ceiling: 21,000 ft (6,400 m)
  • Rate of climb: 1,400 ft/min (7.1 m/s)
  • Time to altitude: 4.5 min to 4,500 ft (1,400 m)

See also

Related development

References

Notes
  1. Flight 31 January 1935, p.118.
  2. Flight 31 January 1935, p.123.
  3. Donald 1997, p.178.
Bibliography
  • Donald, David, ed. (1997). The Encyclopedia of World Aircraft. Leicester, UK: Blitz Editions. ISBN 1-85605-375-X.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985). Orbis Publishing.
  • "Imperial Airways' Latest". Flight. Vol. XXVII no. 1362. 31 January 1935. pp. 118–123.
  • Jackson, A.J. (1974). British Civil Aircraft since 1919. London: Putnam. ISBN 0-370-10014-X.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.