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| Manufacturer | Bell |
| Model | UH-13(H-13) Sioux |
| Modification | Model 47G-4 |
| Country | USA |
| Years | 1948 |
| Type | Helicopter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | - |
| Length | 9.90 m |
| Height | 2.72 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 827 kg |
| Maximum takeoff weight | 1338 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Textron Lycoming VO-540-B1B3 |
| Power | 1 x 227 (209) HP |
| Thrust | - |
| Maximum speed | 169 km/h |
| Cruising speed | 143 km/h |
| Rate of climb | 244 m/min |
| Practical range | 416 km |
| Service ceiling | 3415 m |
| Hovering ceiling | 2345 m |
| Crew | 1 |
