Mac Donnell Douglas DC-10-30
| Entry into service | 1972 |
| Dimensions | Length : 55.5 m |
| Wing span : 50.40 m | |
| Height : 17.7 m | |
| Weights | Maximum take off weight : 259,460 kg |
| Maximum landing weight : 182,766 kg | |
| Operating empty weight : 121,563 kg | |
| Maximum payload : 45,726 kg | |
| Powerplant | 3 x 51,000 - 52,500 lb (23,180 - 23,864 kg) General Electric CF-6-50C/C2. |
| 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 : 2,847 m | |
| Landing field length : 1,758 m | |
| Design range : 10,450 km/277 pax. | |
| Accommodations | 1-class : 380 |
| 2-class : 270 | |
| 3-class : - |