| Attribute | Value |
| General |
| Manufacturer | North American Aviation NAA |
| Model | North American F-100 Super Sabre |
| Country | United States |
| Manufactured from | 1953 year |
| Manufactured to | 1959 year |
| Type | Fighter Jets |
| Icao | F100 |
| Performance |
| Engine | 1x Pratt & Whitney J57-P-21/21A |
| Power, hp | Add |
| Power, lbf | 16,000 lbf |
| Avionics | Minneapolis-Honeywell MB-3, AN/AJB-1B, AN/APR-26 |
| Max cruise speed | 1,487 km/h |
| Approach speed | 300 km/h |
| Travel range | 3,211 km |
| Fuel economy | Add |
| Service ceiling | 15,240 m |
| Rate of climb | 113.79 m/sec |
| Take off distance | Add |
| Landing distance | Add |
| Weights |
| Max take off weight | 15,800 kg |
| Max landing weight | 15,606 kg |
| Max payload | 3,190 kg |
| Fuel tank capacity | 9,887 l |
| Baggage volume | Add |
| Dimensions |
| Seats | 1 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 15 m |
| Tail height | 4.95 m |
| Fuselage diameter | 1.6 m |
| Wing span | 11.8 m |
| Wing tips | No Winglets |