| Manufacturer | McDonnell Douglas |
| Model | F-4 Phantom II |
| Modification | F-4E |
| Country | USA |
| Years | 1961 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11,70 m |
| Length | 19,20 m |
| Height | 5.00. m |
| Wing area | 49,20 m2 |
| Zero fuel weight | - |
| Empty weight | 13760 kg |
| Maximum takeoff weight | 26330. kg |
| Normal takeoff weight | 20800 kg |
| Flight duration | - |
| Engine | 2 xТРДФ General Electric J79-GE-17. |
| Power | - |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 2380 km |
| Service ceiling | 16600 m |
| Hovering ceiling | - |
| Crew | 2 |
