| Manufacturer | McDonnell Douglas |
| Model | MD 520N |
| Modification | MD 520N |
| Country | USA |
| Years | 1990 |
| Type | Helicopter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | - |
| Length | 7.77 m |
| Height | 3.01 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 719 kg |
| Maximum takeoff weight | 1746 kg |
| Normal takeoff weight | 317 kg |
| Flight duration | 2.24 h |
| Engine | 1 Rolls-Royce (Allison) C250-C20R-2 |
| Power | - |
| Thrust | - |
| Maximum speed | 280 km/h |
| Cruising speed | 249 km/h |
| Rate of climb | 564 m/min |
| Practical range | - |
| Service ceiling | 4320 m |
| Hovering ceiling | 2835 m |
| Crew | 1 |
