Jump to content

Caudron C.140

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by TSRL (talk | contribs) at 21:23, 25 March 2015. The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Caudron C.140
Role Liaison and observation and gunnery trainedr
National origin France
Manufacturer Caudron
Designer Paul Deville
First flight 1928

The Caudron C.140 was a French sesquiplane designed in 1928 as a combination of liaison aircraft and observer and gunnery trainer.

Design and development

[1]


Specifications

General characteristics

  • Crew: Two
  • Length: 7.84 m (25 ft 9 in)
  • Upper wingspan: 11.30 m (37 ft 1 in)
  • Lower wingspan: 7.87 m (25 ft 10 in)
  • Height: 2.92 m (9 ft 7 in)
  • Wing area: 28 m2 (300 sq ft)
  • Empty weight: 896 kg (1,975 lb)
  • Gross weight: 1,300 kg (2,866 lb)
  • Fuel capacity: 200 L (44 imp gal; 53 US gal)
  • Powerplant: 1 × Salmson 9AB airc-cooled 9-cylinder radial, 170 kW (230 hp) 230 ch

Performance

  • Maximum speed: 185 km/h (115 mph, 100 kn)
  • Service ceiling: 5,000 m (16,000 ft)

References

  1. ^ Hauet, André (2001). Les Avions Caudrons. Vol. 1. Outreau: Lela Presse. p. 205. ISBN 2 914017-08-1.


Category:Sesquiplanes Category:French military utility aircraft 1920–1929] C.140