(Caudron) Simoun @·AIRCRAFTUBE

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Caudron C.500 - C.620 - C.630 to C.635 Simoun

The Caudron Simoun (Sandstorm) was a 1930s French four-seat touring monoplane designed by Marcel Riffard. It made its maiden flight in 1934 and was first introduced in 1935. It was used as a mail plane by Air Bleu, flew record-setting long-range flights, and was also used as a liaison aircraft by the Armée de l'Air during World War II.

The Simoun was often used as a light transport aircraft and famous pilots used those sport four seaters for fast mail deliveries and also remarkable records, with Tananarive, Hanoï, Saïgon and even the South Atlantic crossing.

Variants

  • C.500 Simoun I - experimental, one was built.
  • C.520 Simoun - experimental, one was built.
  • C.620 Simoun IV - experimental, one was built.
  • C.630 Simoun - initial production version with Renault Bengali 6Pri engine, 20 were built.
  • C.631 Simoun - modified version with a Renault Bengali 6Q-01 engine, three were built.
  • C.632 Simoun - similar to C.631, one was built.
  • C.633 Simoun - modified fuselage with a Renault Bengali 6Q-07 engine, 6 were built.
  • C.634 Simoun - modified wing and take-off weight with either a Renault Bengali 6Q-01 or Renault Bengali 6Q-09 engine, 3 were built.
  • C.635 Simoun - improved cabin layout and either a Renault Bengali 6Q-01 or Renault Bengali 6Q-09 engine, 46 were built and conversions were done from earlier versions.
  • C.635M Simoun - military version with either a Renault Bengali 6Q-09 or Renault Bengali 6Q-19 engine, 489 were built.

Operators

In France: Air Bleu and the Armée de l'Air. In Germany: The Luftwaffe. In the United States: The United States Navy.

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This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Caudron Simoun of Wikipedia ( authors )

Specifications (C.630)

  • Crew : 1-2 : pilot and (optional) co-pilot.
  • Capacity : 2 passengers.
  • Length : 9.10 m (or 29 ft 10 in).
  • Height : 2.3 m (or 7 ft 7 in).
  • Wingspan : 10.4 m (or 34 ft 2 in).
  • Wing area : 16 m² (or 170 ft²).
  • Empty weight : 755 kg (or 1,660 lb).
  • Max. takeoff weight : 1,380 kg (or 3,040 lb).
  • Max. speed : 300 km/h (or 160 knots or 190 mph).
  • Range : 1,500 km (or 810 nm or 930 mi).
  • Service ceiling 6,000 m (or 20,000 ft)
  • Powerplant : One Renault Bengali 6Q-09 six-cylinder inline engine.
  • Power : 220 hp (or 160 kW).

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This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Caudron Simoun of Wikipedia ( authors )
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