| Manufacturer | Boeing |
| Model | C-135 Stratolifter |
| Modification | C-135A |
| Country | USA |
| Years | 1961 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 39.88 m |
| Length | 41.53 m |
| Height | 12.70 m |
| Wing area | 226.03 m2 |
| Zero fuel weight | - |
| Empty weight | 44664 kg |
| Maximum takeoff weight | 143335 kg |
| Normal takeoff weight | 136806 kg |
| Flight duration | - |
| Engine | 4 Pratt Whitney J57-P-59W |
| Power | - |
| Thrust | - |
| Maximum speed | 982 km/h |
| Cruising speed | 888 km/h |
| Rate of climb | - |
| Practical range | 14806 km |
| Service ceiling | 13715 m |
| Hovering ceiling | - |
| Crew | 5 |
