| Manufacturer | Boeing |
| Model | VC-137 Stratoliner |
| Modification | VC-137В |
| Country | USA |
| Years | 1962 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 44.17 m |
| Length | 46.33 m |
| Height | 12.91 m |
| Wing area | 279.64 m2 |
| Zero fuel weight | - |
| Empty weight | 61236 kg |
| Maximum takeoff weight | 144900 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 4 Pratt Whitney JT3D-3В |
| Power | - |
| Thrust | 4 x 8100 kN |
| Maximum speed | - |
| Cruising speed | 981 km/h |
| Rate of climb | - |
| Practical range | 12400 km |
| Service ceiling | 12727 m |
| Hovering ceiling | - |
| Crew | 3 + 15 обслуживающего персонала |
