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Caudron C.440 Goéland

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Top speed
  
300 km/h

Length
  
14 m

Manufacturer
  
Wingspan
  
18 m

First flight
  
1934

Designer
  
Caudron C.440 Goéland httpswwwaviationsmilitairesnetmediapictures

The Caudron C.440 Goéland ("seagull") was a six-seat twin-engine utility aircraft developed in France in the mid-1930s.

Contents

Design and development

Caudron C.440 Goéland Caudron C440 Goland

It was a conventionally configured low-wing cantilever monoplane with tailwheel undercarriage. The main undercarriage units retracted into the engine nacelles. Construction was wooden throughout, with wooden skinning everywhere but the forward and upper fuselage sections, which were skinned in metal. As usually configured, the cabin seated six passengers with baggage compartments fore and aft, and a toilet aft.

Operation history

Caudron C.440 Goéland Caudron C440 Goland avionslegendairesnet

Apart from private buyers, the C.440 was also bought by the Armée de l'Air, Aéronavale, Aéromaritime, Régie Air Afrique and Air France, and some were exported for service with Aeroput. Production of the C.440 and its subtypes continued until the outbreak of World War II, at which time many C.440s were impressed into military service. Following the fall of France, some were operated by the German Luftwaffe and Deutsche Luft Hansa. Another user was the Slovenské vzdušné zbrane - it ordered 12 aircraft as the C.445M in 1942.

Caudron C.440 Goéland Caudron C440 Goland Tous les avions militaires

Production was restarted following the war for both military and civil use as a transport and as a twin-engined trainer. In the postwar reorganisation of the French aircraft industry, Caudron became part of SNCA du Nord, and the aircraft became the Nord Goeland; 325 of these were built. Postwar commercial operators included Air France, SABENA, Aigle Azur, and Compagnie Air Transport (CAT).

Variants

Caudron C.440 Goéland Caudron C440 Goland Wikipedia

  • C.440 - prototype (three built)
  • C.441 - version with Renault 6Q-01 engine and dihedral added to outer wing panel (four built)
  • C.444 - first version with counter-rotating propellers, adopted on all later versions (17 built)
  • C.445 - similar to C.444, but dihedral of outer wing panels increased (114 built)
  • C.445/1 - two built
  • C.445/2 - three built
  • C.445/3 - postwar production version (510 built)
  • C.445M - militarised version (404 built)
  • C.445R - long-range version (one built)
  • C.446 Super Goéland - one built
  • C.447 - air ambulance version (31 built)
  • C.448 - version with supercharged engines (seven built)
  • C.449 - final production version (349 built, including subtypes below)
  • C.449/1
  • C.449/2
  • C.449/3
  • C.449/4 - photographic survey version
  • C.449/5
  • Operators

     Belgium
  • Belgian Air Force
  • SABENA
  •  Bulgaria
  • Bulgarian Air Force
  •  France
  • Air Bleu
  • Aéromaritime
  • Aeronavale
  • Aigle Azur
  • Air France
  • Armee de l'Air
  • Compagnie Air Transport (CAT)
  • Règie Air Afrique
  •  Germany
  • Deutsche Luft Hansa
  • Luftwaffe
  •  Yugoslavia
  • Aeroput
  • Royal Yugoslav Air Force - One aircraft was impressed into military in April 1940.
  •  Slovakia
  • Slovenské vzdušné zbrane
  •  Spain
  • LAPE
  • Spanish Republican Air Force
  • Specifications (C.445M)

    General characteristics

    Caudron C.440 Goéland Caudron C440 Goeland military transport or trainer

  • Crew: two pilots
  • Length: 13.68 m (44 ft 11 in)
  • Wingspan: 17.59 m (57 ft 9 in)
  • Height: 3.40 m (11 ft 2 in)
  • Wing area: 42.0 m2 (452 ft2)
  • Empty weight: 2,292 kg (5,053 lb)
  • Gross weight: 3,500 kg (7,716 lb)
  • Powerplant: 2 × Renault 6Q, 164 kW (220 hp) each
  • Performance

    Caudron C.440 Goéland Caudron C440 Goland

  • Maximum speed: 300 km/h (186 mph)
  • Range: 1,000 km (620 miles)
  • Service ceiling: 7,000 m (22,965 ft)
  • Rate of climb: 3.3 m/s (650 ft/min)
  • References

    Caudron C.440 Goéland Wikipedia