| Manufacturer | Caudron |
| Model | CR.714 Cyclone |
| Modification | CR.714 |
| Country | France |
| Years | 1938 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 8.97 m |
| Length | 8.53 m |
| Height | 2.87 m |
| Wing area | 12.50 m2 |
| Zero fuel weight | - |
| Empty weight | 1400 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 1750 kg |
| Flight duration | - |
| Engine | 1 Renault 12Ro1 |
| Power | 1 x 450 HP |
| Thrust | - |
| Maximum speed | 485 km/h |
| Cruising speed | 320 km/h |
| Rate of climb | - |
| Practical range | 900 km |
| Service ceiling | 9100 m |
| Hovering ceiling | - |
| Crew | - |
