Mac Donnell - Douglas DC-8-61
| Entry into service | 1967 |
| Dimensions | Length : 57.12 m |
| Wing span : 43.41 m | |
| Height : 12.92 m | |
| Weights | Maximum take off weight : 147,415 kg |
| Maximum landing weight : 108,860 kg | |
| Operating empty weight : 67,538 kg | |
| Maximum payload : 30,240 kg | |
| Powerplant | 4 x 18,000 lb (8,172 kgp) Pratt & Whitney JT3D-3B |
| Fuel capacity | 88,531 l |
| Performance | Maximum cruise speed : 521 kt - 965 km/h |
| Maximum cruising altitude : 42,000 ft - 12,730 m | |
| T-O distance : 3,042 m | |
| Landing field length : 1,870 m | |
| Design range :6,035 km/259 pax. | |
| Accommodations | 1-class : 259 |
| 2-class : | |
| 3-class : |