| First Flight date: | ||
| Certification date: | 12 Feb 1990 |
| Fuselage width: | 3.76 m | |
| Fuselage height: | 4.01 m | |
| Fuselage length: | 29.79 m | |
| Cabin length: | 21.79 m | |
| Cabin width: | 3.54 m | |
| Cabin height: | 2.15 m | |
| Cabin volume: | ||
| Hold volume: | 23 m3 |
| Empty operating: | 31,300 kg | |
| Max zero fuel: | 46,500 kg | |
| MTOW: | 60,550 kg | |
| MLW: | 49,900 kg | |
| Standard fuel capacity: | 20,104 kg | |
| Max fuel capacity: | 20,104 kg |
| Normal cruise: | 795 km/h | |
| Max cruise: | 910 km/h |
| Long Range Cruise alt: | 10,668 m | |
| Max ceiling: | 11,278 m | |
| Take off field length: | 1,804 m | |
| Landing field length: | 1,340 m | |
| Max Payload Range: | ||
| Range notes: | ||
| Max passengers: | 132 | |
| Typical passengers: | 110 |
| Category: | Turbofan | |
| Manufacturer: | CFM International | |
| Model/Submodel: | CFM56 3B1 | |
| Thrust: | 89 kN |
| Category: | Turbofan | |
| Manufacturer: | CFM International | |
| Model/Submodel: | CFM56 3 | |
| Thrust: | 104 kN |