| Manufacturer | Boeing) |
| Model | C-17 Globemaster III |
| Modification | C-17A |
| Country | USA |
| Years | 1991 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 50.29 m |
| Length | 53.04 m |
| Height | 16.79 m |
| Wing area | 353.02 m2 |
| Zero fuel weight | 122016 kg |
| Empty weight | - |
| Maximum takeoff weight | 263083 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 4 Pratt Whitney F117-P-100 |
| Power | - |
| Thrust | 4 x 185.49 kN |
| Maximum speed | 830 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 4450 km |
| Service ceiling | 13700 m |
| Hovering ceiling | - |
| Crew | 3-4 |
