| Manufacturer | North American |
| Model | F-100A(B) Super Sabre |
| Modification | F-100A |
| Country | USA |
| Years | 1953 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11,82 m |
| Length | 14,33 m |
| Height | 4,94 m |
| Wing area | 37,18 m2 |
| Zero fuel weight | - |
| Empty weight | 9100 kg |
| Maximum takeoff weight | 16578 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 ТРД Pratt Whitney J57-P-21 |
| Power | - |
| Thrust | - |
| Maximum speed | 1448 km/h |
| Cruising speed | 966 km/h |
| Rate of climb | - |
| Practical range | 2173 km |
| Service ceiling | 15545 m |
| Hovering ceiling | - |
| Crew | 1 |
