| Manufacturer | McDonnell Douglas |
| Model | MD-11 |
| Modification | MD-11 |
| Country | USA |
| Years | 1990 |
| Type | Passenger aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 51.60 m |
| Length | 61.20 m |
| Height | 17.60 m |
| Wing area | 338.90 m2 |
| Zero fuel weight | 125870 kg |
| Empty weight | - |
| Maximum takeoff weight | 277300 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 3 General Electric CF6-80C2D1F (Pratt Whitney PW4460) |
| Power | - |
| Thrust | 3 x 273 (267) kN |
| Maximum speed | 962 km/h |
| Cruising speed | 912 km/h |
| Rate of climb | - |
| Practical range | 9270 km |
| Service ceiling | 9935 m |
| Hovering ceiling | - |
| Crew | 2 |
