| Manufacturer | Sud-Aviation |
| Model | SE.210 Caravelle 1 |
| Modification | Caravelle I |
| Country | France |
| Years | 1955 |
| Type | Passenger aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 34.30 m |
| Length | 32.01 m |
| Height | 8.72 m |
| Wing area | 146.70 m2 |
| Zero fuel weight | - |
| Empty weight | 23400 kg |
| Maximum takeoff weight | 43500 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 ТРД Rolls-Royce Avon RA.29 Mk 522 |
| Power | - |
| Thrust | 2 x 4760 kN |
| Maximum speed | 800 km/h |
| Cruising speed | 734 km/h |
| Rate of climb | - |
| Practical range | 1850 km |
| Service ceiling | 10000 m |
| Hovering ceiling | - |
| Crew | 3 |
