Airbus A.300B4-200
| Entry into service | May 1974 |
| Dimensions | Length : 53.75 m |
| Wing span : 44,84 m | |
| Height : 16,53 m | |
| Weights | Maximum take off weight : 165 000 kg |
| Maximum landing weight : 134 000 kg | |
| Operating empty weight : 80 640 kg | |
| Maximum payload : 25 500 kg | |
| Powerplant | 2 x 52 350 lb GE CF6-50C |
| 2 x 53 000 lb P&W JT9D-59A1 | |
| Fuel capacity | Standard : 62 000 l |
| Performance | Maximum cruise speed : 480 kt - 889 km/h |
| Maximum cruising altitude : 35 000 ft - 10 667 m | |
| Design range : 5 270 km with 251 pax. | |
| Accommodations | 1-class : 345 |
| 2-class : 254 | |
| 3-class : - |