| Manufacturer | Boeing |
| Model | C-137 Stratoliner |
| Modification | C-137B |
| Country | USA |
| Years | 1958 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 44.42 m |
| Length | 46.61 m |
| Height | 12.93 m |
| Wing area | 279.64 m2 |
| Zero fuel weight | - |
| Empty weight | 61236 kg |
| Maximum takeoff weight | 148325 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 4 Pratt Whitney TF33 (JT3D-3) |
| Power | - |
| Thrust | 4 x 80.07 kN |
| Maximum speed | 1010 km/h |
| Cruising speed | 966 km/h |
| Rate of climb | - |
| Practical range | 12248 km |
| Service ceiling | 12800 m |
| Hovering ceiling | - |
| Crew | 3-4 |
