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SABCA S.40

From Wikipedia, the free encyclopedia
S.40
3-views of the SABCA S.40E
Role Trainer
National origin Belgium
Manufacturer SABCA
First flight 1939

The SABCA S.40 was a military trainer aircraft built in Belgium in 1939.[1]

Design and development

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The S.40 was a graceful, low-wing cantilever monoplane of conventional design with fixed, tailwheel undercarriage. The pilot and instructor sat in tandem cockpits, enclosed by sliding canopies.[2] A single engine driving a two-blade propeller was mounted in the nose. The main undercarriage units were fully independent, mounted under the wings, and enclosed in spats. A small number were built for the Belgian military before the German invasion in 1940.[2]

Specifications

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General characteristics

  • Crew: two, pilot and instructor
  • Length: 7.14 m (23 ft 5 in)
  • Wingspan: 10.20 m (33 ft 6 in)
  • Height: 2.40 m (7 ft 11 in)
  • Empty weight: 780 kg (1,720 lb)
  • Gross weight: 1,240 kg (2,730 lb)
  • Powerplant: 1 × Renault 4Pei , 104 kW (140 hp)

Performance

  • Maximum speed: 360 km/h (230 mph, 200 kn)

Notes

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  1. ^ Taylor 1989, p.787
  2. ^ a b The Illustrated Encyclopedia of Aircraft, p.2837

References

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  • The Illustrated Encyclopedia of Aircraft. London: Aerospace Publishing.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.