| Manufacturer | Douglas |
| Model | C-118 Liftmaster |
| Modification | C-118A |
| Country | USA |
| Years | 1947 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 35.81 m |
| Length | 32.56 m |
| Height | 8.74 m |
| Wing area | 135.92 m2 |
| Zero fuel weight | - |
| Empty weight | 23358 kg |
| Maximum takeoff weight | 48534 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 4 Pratt Whitney R-2800-52W |
| Power | 4 x 2500 HP |
| Thrust | - |
| Maximum speed | 573 km/h |
| Cruising speed | 504 km/h |
| Rate of climb | - |
| Practical range | 6184 km |
| Service ceiling | 8505 m |
| Hovering ceiling | - |
| Crew | 4 |
