Mac Donnell Douglas MD-11
| Entry into service | 1990 | |
| Dimensions | Length : 61.60 m | |
| Wing span : 51.70 m | ||
| Height : 17.65 m | ||
| Weights | Maximum take off weight : | 259,460 kg |
| Option : 286,250 kg (MD-11ER) | ||
| Maximum landing weight : 195,050 kg | ||
| Operating empty weight : 132,800 kg | ||
| Maximum payload : 62,248 kg | ||
| Powerplant |
3 x 60,000 lb (27,270 kgp) Pratt&Whitney PW4460. or 3 x 61,970 lb (28,170 kgp) Pratt&Whitney PW4462. 3 x 61,340 lb (27,880 kg) General Electric CF-6-80C2. |
|
| Fuel capacity | 146,174 l | |
| Option : 165,290 (MD-11ER) | ||
| Performance | Maximum cruise speed : 511 kt - 946 km/h | |
| Maximum cruising altitude : 42,000 ft - 13,030 m | ||
| T-O distance : 3,115 m | ||
| Landing field length : 2,118 m | ||
| Design range : | 12,270 km/285 pax. | |
| Option : 13,340 km/298 pax. | ||
| Accommodations | 1-class : 410 | |
| 2-class : 356 | ||
| 3-class : 285 | ||