Airbus A.320-200
| Entry into service | 1988 | |
| Dimensions | Length : 37.58 m | |
| Wing span : 34.10 m | ||
| Height : 11.76 m | ||
| Weights | Maximum take off weight : | 73,500 kg |
| Option :75,000 kg | ||
| Option :77,000 kg | ||
| Maximum landing weight : | 64,500 kg | |
| Option : 66,000 kg | ||
| Operating empty weight : 42,100 kg | ||
| Maximum payload : 18,600 kg | ||
| Powerplant | 2 x 25,000 - 26,500 lb GE CFM-56-5A or -5B | |
| 2 x 25,000 - 26,500 lb IAE V2500-A5 | ||
| Fuel capacity | Standard : 23,860 l | |
| Option : 26,850 l | ||
| Option : 29,840 l | ||
| Performance | Maximum cruise speed : 470 kt - 871 km/h | |
| Maximum cruising altitude : 39,000 ft - 11,887 m | ||
| Design range : 5,350 km with 150pax./Option : 5,550 km | ||
| Accommodations | 1-class : 180 | |
| 2-class : 150 | ||
| 3-class : - | ||