| Manufacturer | McDonnell Douglas |
| Model | F-4C Phantom II |
| Modification | F-4С |
| Country | USA |
| Years | 1963 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11,68 m |
| Length | 17,75 m |
| Height | 4,95 m |
| Wing area | 48,40 m2 |
| Zero fuel weight | - |
| Empty weight | 13200 kg |
| Maximum takeoff weight | 24766 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 ТРД General Electric J79-GE-15 |
| Power | - |
| Thrust | - |
| Maximum speed | 2390 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 2590 km |
| Service ceiling | 18900 m |
| Hovering ceiling | - |
| Crew | - |
