Airbus A.321-100/200
| Entry into service | March 1994 | |
| Dimensions | Length : 44.51 m | |
| Wing span : 34.10 m | ||
| Height : 11.76 m | ||
| Weights | Maximum take off weight : | 83,000 kg |
| Option :85,000 kg | ||
| Option :89,000 kg | ||
| Option : 93 500 kg | ||
| Maximum landing weight : | 76,500 kg | |
| Option : 77,800 kg | ||
| Operating empty weight : 48,080 kg | ||
| Maximum payload : 23,420 kg | ||
| Powerplant | 2 x 30,000 - 33,000 lb GE CFM-56-5A or -5B | |
| 2 x 30,000 - 33,000 lb IAE V2500-A5 | ||
| Fuel capacity | Standard : 23,760 l | |
| Option : 26,690 l | ||
| Option : 29,680 l | ||
| Performance | Maximum cruise speed : 470 kt - 871 km/h | |
| Maximum cruising altitude : 39,000 ft - 11,887 m | ||
| Design range : 5,000 km with 185 pax./Option : 5,550 km | ||
| Accommodations | 1-class : 220 | |
| 2-class : 185 | ||
| 3-class : - | ||