| Manufacturer | Gulfstream |
| Model | VC-11 |
| Modification | VC-11 |
| Country | USA |
| Years | 1968 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 20.98 m |
| Length | 24.36 m |
| Height | 7.47 m |
| Wing area | 73.72 m2 |
| Zero fuel weight | - |
| Empty weight | 13772 kg |
| Maximum takeoff weight | 29711 kg |
| Normal takeoff weight | 26081 kg |
| Flight duration | - |
| Engine | 2 Rolls-Royce Spey RB.168 Mk 511-8 |
| Power | - |
| Thrust | 2 x 50.71 kN |
| Maximum speed | 941 km/h |
| Cruising speed | 909 km/h |
| Rate of climb | - |
| Practical range | 5568 km |
| Service ceiling | 13105 m |
| Hovering ceiling | - |
| Crew | 2-3 |
