Blackburn Cirrus Bombardier

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Cirrus Bombardier
Blackburn Bombardier.JPG
Type Air-cooled 4-cylinder inline piston engine
National origin United Kingdom
Manufacturer Blackburn Aircraft
First run c.1954

The Blackburn Cirrus Bombardier was a British four-cylinder inline aircraft engine, developed and built by the Blackburn Aircraft company in the mid-1950s. The engine featured fuel injection.

Variants[edit]

Cirrus Bombardier 203
Military version, 203 hp (151 kW).
Cirrus Bombardier 702
Civil version, 180 hp (134 kW).

Applications[edit]

Specifications (Cirrus Bombardier 203)[edit]

Data from Lumsden.[1]

General characteristics

  • Type: Air-cooled, inline inverted four-cylinder
  • Bore: 4.8 in (122 mm)
  • Stroke: 5.5 in (140 mm)
  • Displacement: 398 cu in (6.5 L)
  • Length: 45.3 in (1,151 mm)
  • Width: 19 in (483 mm)
  • Height: 30.95 in (786 mm)
  • Dry weight: 325 lb (147.4 kg)

Components

Performance

See also[edit]

Related development
Comparable engines
Related lists

References[edit]

Notes[edit]

  1. ^ Lumsden 2003, p.91.

Bibliography[edit]

  • Oldengine.org
  • Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 40. 
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.

External links[edit]