Caudron C.230

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C.230
300px
C.232 partly visible in a background, during the Challenge 1930 competition
Role Touring
Manufacturer Caudron
Designer Paul Deville
First flight 1930
Number built 15

The Caudron C.230 was a sporting, touring and trainer aircraft produced in France in 1930. It was a conventional biplane with single-bay, unstaggered wings of equal span. The pilot and a single passenger sat in tandem open cockpits. It featured a wooden fuselage with plywood skin.

Fifteen examples were produced before the much improved and very successful Caudron C.270 Luciole series appeared.

Variants

  • C.230 - first production version with Salmson 7Ac radial engine (15 built)
  • C.232 - version with Renault 4Pb engine (50 built)
    • C.232/2 - as C.232 with wheel brakes (3 built)
    • C.232/4 - as C.232/2 with improved equipment (7 built)
  • C.233 - prototype for testing of Michel AM-16 engine, later re-engined with Salmson 7Ac, reverting to C.230 designation. (1 built)
  • C.235 - version with Argus As 8R engine for French Air Ministry (Ministere de l'Air) tests (1 built)


Specifications (C.232)

General characteristics

  • Crew: 1, pilot
  • Capacity: 1 passenger
  • Length: 7.87 m (25 ft 10 in)
  • Wingspan: 11.00 m (36 ft 1 in)
  • Wing area: 24.0 m2 (258 ft2)
  • Empty weight: 420 kg (926 lb)
  • Gross weight: 700 kg (1543 lb)
  • Powerplant: 1 × Renault 4Pb, 71 kW (95 hp)

Performance

  • Maximum speed: 165 km/h (102.5 mph)
  • Range: 500 km (311 miles)
  • Service ceiling: 4,000 m (13,120 ft)

References

External links