| Manufacturer | McDonnell Douglas |
| Model | F-15A-B Eagle |
| Modification | F-15A |
| Country | USA |
| Years | 1974 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 13,05 m |
| Length | 19,05 m |
| Height | 5.63 m |
| Wing area | 56,6 m2 |
| Zero fuel weight | - |
| Empty weight | 12970 kg |
| Maximum takeoff weight | 30850 kg |
| Normal takeoff weight | 18820 kg |
| Flight duration | - |
| Engine | 2 Ф Pratt Whitney F100-PW-100 |
| Power | - |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 18300 m |
| Hovering ceiling | - |
| Crew | - |
