Douglas DC-8 (10/20/30/40)
| Entry into service | 1959 | |
| Dimensions | Length : 45.87 m | |
| Wing span : 43.41 m | ||
| Height : 12.91 m | ||
| Weights | Maximum take off weight : 123,230 kg | |
| Maximum landing weight : | ||
| Operating empty weight : 64,884 kg | ||
| Maximum payload : | ||
| Powerplant | DC-8-10 | 4 x 13,472 lb P&W JT3C-6 |
| DC-8-20 | 4 x 15,679 lb P&W JT4A-3 | |
| 4 x 16,764 lb P&W JT4A-9 | ||
| 4 x 17,762 lb Rolls Royce Conway RCo 12. | ||
| 4 x 18,480 lb Rolls Royce Conway RCo 15. | ||
| Fuel capacity | ||
| Performance | Maximum cruise speed : 482 kt - 893 km/h | |
| Maximum cruising altitude : | ||
| Design range : 6,630 km | ||
| Accommodations | 1-class : - | |
| 2-class : - | ||
| 3-class : - | ||