| Manufacturer | Boeing |
| Model | C-40 Clipper |
| Modification | C-40A |
| Country | USA |
| Years | 2001 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 34.3 m |
| Length | 33.6 m |
| Height | 12.5 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 83790 kg |
| Maximum takeoff weight | 154500 kg |
| Normal takeoff weight | 133000 kg |
| Flight duration | - |
| Engine | 2 General Electric CFM56-7B |
| Power | - |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | 850 km/h |
| Rate of climb | - |
| Practical range | 6110 km |
| Service ceiling | 9800 m |
| Hovering ceiling | - |
| Crew | 2-3 |
