Designed by Marcel Riffard, the Caudron C.714 (often called Cyclone) was developed as a lightweight fighter, one of the few to achieve production and actually serve in World War II. It was based on a series of racing aircraft of mostly wooden construction made for a quite economical fighter which could be built rapidly in large numbers. Unfortunately, the light fighter concept proved significantly flawed and only a small number ended up in service, mostly with some Polish volunteer training squadrons which flew against the Luftwaffe, claiming 12 aircraft destroyed at a cost of 13 of their own. After the surrender, a small number were used by Vichy forces while others were taken over and used by the Luftwaffe; a few partly assembled units were also sent to Finland, part of a larger order which was interrupted by the capitulation although one squadron was formed.
First flight of the prototype C.714 took place on 6 July 1938, it had been based on the earlier C.710 lightweight fighter and the C.713 fighter with retractable landing gear and a redigned vertail tail surfaces. The C.714 was the main production version armed with wing-mounted machine-guns while other planned developments featured more powerful engines but none ever reached production.
Preceded by:
NoneSucceeded by:
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Design | C.714 |
Type | Fighter |
Year | 1939 |
Crew | 1 |
Dimensions | |
Length | 8.63 m |
Height | 2.870 m |
Wing Span | 8.97 m |
Wing Area | n/a |
Weight | |
Empty | 1,400 kg |
Maximum | 1,880 kg |
Wing Loading | 150.4 kg/m² |
Performance | |
Speed | 486 km/h |
Ceiling | 9,100 m |
Range | 900 km |
Powerplant | |
Engine | 1 x 12R 03 Renault 336 kW |
Thrust/Weight | 0.29 |
Armament | |
Guns | 4 x 7.5-mm |
Payload | - |
Production | |
Built | 90 |
Total | 91 |