Airbus A.310-200
| Entry into service | 1983 |
| Dimensions | Length : 46,66 m |
| Wing span : 43,90m | |
| Height : 15,80 m | |
| Weights | Maximum take off weight : 142 000 kg |
| Maximum landing weight : 123 000 kg | |
| Operating empty weight : 90 300 kg | |
| Maximum payload : 33 550 kg | |
| Powerplant | 2 x GE 52 320 lb CF6-80C2A2 |
| 2 x 53 000 lb P&W JT9D-59A1 | |
| Fuel capacity | Standard : 54 920 l |
| Performance | Maximum cruise speed : 484 kt - 896 km/h |
| Maximum cruising altitude : 40 000 ft - 12 191 m | |
| Design range : 4 633 km with 220 pax. | |
| Accommodations | 1-class : 279 |
| 2-class : 218 | |
| 3-class : 187 |