| Manufacturer | Gulfstream |
| Model | C-20 Gulfstream IV |
| Modification | С-20А |
| Country | USA |
| Years | 1987 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 23.72 m |
| Length | 26.92 m |
| Height | 7.57 m |
| Wing area | 88.29 m2 |
| Zero fuel weight | - |
| Empty weight | 16102 kg |
| Maximum takeoff weight | 33203 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 Rolls-Royce Tay RB.183 Mk 611-8 |
| Power | - |
| Thrust | 2 x 61.61 kN |
| Maximum speed | - |
| Cruising speed | 943 km/h |
| Rate of climb | - |
| Practical range | 7820 km |
| Service ceiling | 13715 m |
| Hovering ceiling | - |
| Crew | 2-3 |
