| Manufacturer | McDonnell Douglas |
| Model | MD 500E |
| Modification | MD 500E (с Allison 250-C20R ) |
| Country | USA |
| Years | 1982 |
| Type | Helicopter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | - |
| Length | 7.49 m |
| Height | 2.97 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 672 (688) kg |
| Maximum takeoff weight | 1610 kg |
| Normal takeoff weight | 280 kg |
| Flight duration | - |
| Engine | 1 Rolls-Royce (Allison) 250-C20B (Allison 250-C20R) |
| Power | - |
| Thrust | - |
| Maximum speed | 282 km/h |
| Cruising speed | 249 km/h |
| Rate of climb | 540 m/min |
| Practical range | 488 (478) km |
| Service ceiling | 4877 m |
| Hovering ceiling | 2590 m |
| Crew | 1 |
