Mac Donnell Douglas DC-10-40
| Entry into service | 1972 |
| Dimensions | Length : 55.5 m |
| Wing span : 50.40 m | |
| Height : 17.7 m | |
| Weights | Maximum take off weight : 259,450 kg |
| Maximum landing weight : 182,798 kg | |
| Operating empty weight : 121,220 kg | |
| Maximum payload : 45,700 kg | |
| Powerplant | 3 x 49,000 - 51,000 lb (22,226 - 23,133 kg) General Electric CF-6-50A/C. |
| Fuel capacity | 138,904 l |
| Performance | Maximum cruise speed : 530 kt - 982 km/h |
| Maximum cruising altitude : 42,000 ft - 13,030 m | |
| T-O distance : 3,444 m | |
| Landing field length :1,836 m | |
| Design range : 11,305 km/- t payload. | |
| Accommodations | 1-class : 380 |
| 2-class : 270 | |
| 3-class : - |