Airbus A.318-100
| Entry into service | May 1999 | |
| Dimensions | Length : 33.84 m | |
| Wing span : 34.10 m | ||
| Height : 11.76 m | ||
| Weights | Maximum take off weight : | 64,000 kg |
| Option :68,000 kg | ||
| Option :70,000 kg | ||
| Option : 75,500 kg | ||
| Maximum landing weight : | 61,000 kg | |
| Option : 62,500 kg | ||
| Operating empty weight : 40,300 kg | ||
| Maximum payload : 17,900 kg | ||
| Powerplant | 2 x 22,000 - 23,350 lb GE CFM-56-5A or -5B | |
| 2 x 22,000 - 23,500 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 : 4,700 km with 124 pax./Option : 6 800 km | ||
| Accommodations | 1-class : 150 | |
| 2-class : 124 | ||
| 3-class : - | ||