| Manufacturer | McDonnell Douglas |
| Model | Phantom FG.Mk.1 |
| Modification | Phantom FG.Mk.1 |
| Country | USA |
| Years | 1964 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.70 m |
| Length | 17.55 m |
| Height | 4.96 m |
| Wing area | 49.20 m2 |
| Zero fuel weight | - |
| Empty weight | 13800 kg |
| Maximum takeoff weight | 26800 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 ТРДФ Rolls-Royce Spey 202 Mk.202 |
| Power | - |
| Thrust | 2 x 9305 kN |
| Maximum speed | 2230 km/h |
| Cruising speed | 980 km/h |
| Rate of climb | - |
| Practical range | 2817 km |
| Service ceiling | 18300 m |
| Hovering ceiling | - |
| Crew | - |
