Mac Donnell Douglas DC-10-30F
| Entry into service | 1996 |
| Dimensions | Length : 55.5 m |
| Wing span : 50.40 m | |
| Height : 17.7 m | |
| Weights | Maximum take off weight : 263,300 kg |
| Maximum landing weight : 197,770 kg | |
| Operating empty weight : 106,505 kg | |
| Maximum payload : 73,030 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 : - m | |
| Landing field length : - m | |
| Design range : 5,735 km/73 t payload. | |
| Accommodations | 1-class : - |
| 2-class : - | |
| 3-class : - |