Airbus A.318-100
| Entry into service | July 2003 | |
| Dimensions | Length : 31.44 m | |
| Wing span : 34.10 m | ||
| Height : 12.56 m | ||
| Weights | Maximum take off weight : | 59,000 kg |
| Option :63,000 kg | ||
| Option :66,000 kg | ||
| Option : 68,000 kg | ||
| Maximum landing weight : | 56,000 kg | |
| Option : 57,000 kg | ||
| Operating empty weight : 39,470 kg | ||
| Maximum payload : 13,340 kg | ||
| Powerplant | 2 x GE 21,600 - 23,300 lb CFM-56-5B | |
| 2 x 22,100 - 23,800 lb P&W JT9D-59A1 | ||
| Fuel capacity | Standard : 23,860 l | |
| Performance | Maximum cruise speed : 470 kt - 871 km/h | |
| Maximum cruising altitude : 39,000 ft - 11,887 m | ||
| Design range : 2,750 km with 107 pax. | ||
| Accommodations | 1-class : 117 | |
| 2-class : 107 | ||
| 3-class : - | ||