| Manufacturer | McDonnell Douglas |
| Model | MD-11F |
| Modification | MD-11F |
| Country | USA |
| Years | 1990 |
| Type | Passenger aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 51.97 m |
| Length | 61.62 m |
| Height | 17.60 m |
| Wing area | 338.90 m2 |
| Zero fuel weight | 113920 kg |
| Empty weight | - |
| Maximum takeoff weight | 285990 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 3 General Electric CF6-80C2D1F (Pratt Whitney PW4462) |
| Power | - |
| Thrust | 3 x 274 (276) kN |
| Maximum speed | 945 km/h |
| Cruising speed | 890 km/h |
| Rate of climb | - |
| Practical range | 7800 km |
| Service ceiling | 9850 m |
| Hovering ceiling | - |
| Crew | 2 |
