| Manufacturer | McDonnell Douglas |
| Model | MD-90-30 |
| Modification | MD-90-30 |
| Country | USA |
| Years | 1993 |
| Type | Passenger aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 32.87 m |
| Length | 46.51 m |
| Height | 9.33 m |
| Wing area | 112.30 m2 |
| Zero fuel weight | 39900 kg |
| Empty weight | - |
| Maximum takeoff weight | 70700 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 International Aero Engines V2525-D5 |
| Power | - |
| Thrust | 2 x 11350 kN |
| Maximum speed | 875 km/h |
| Cruising speed | 810 km/h |
| Rate of climb | - |
| Practical range | 4200 km |
| Service ceiling | 10670 m |
| Hovering ceiling | - |
| Crew | 2 |
