| Manufacturer | Piasecki |
| Model | CH-25 Army Mule |
| Modification | CH-25A |
| Country | USA |
| Years | 1948 |
| Type | Transport helicopter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | - |
| Length | 17.35 m |
| Height | 3.81 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 1782 kg |
| Maximum takeoff weight | 2767 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Continental R-975-46А |
| Power | 1 x 410 HP |
| Thrust | - |
| Maximum speed | 174 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 790 km |
| Service ceiling | 3670 m |
| Hovering ceiling | - |
| Crew | 1 |
