| First Flight date: | 22 Feb 1987 | |
| Certification date: | 8 Nov 1988 |
| Fuselage width: | 3.96 m | |
| Fuselage height: | 6 m | |
| Fuselage length: | 37.57 m | |
| Cabin length: | 27.51 m | |
| Cabin width: | 3.7 m | |
| Cabin height: | 2.13 m | |
| Cabin volume: | 139 m3 | |
| Hold volume: | 44 m3 |
| Empty operating: | 42,100 kg | |
| Max zero fuel: | 61,000 kg | |
| MTOW: | 73,500 kg | |
| MLW: | 64,500 kg | |
| Standard fuel capacity: | 23,859 kg | |
| Max fuel capacity: | 53,699 kg |
| Normal cruise: | 811 km/h | |
| Max cruise: | 875 km/h |
| Long Range Cruise alt: | 10,668 m | |
| Max ceiling: | 12,131 m | |
| Take off field length: | 2,158 m | |
| Landing field length: | 1,899 m | |
| Max Payload Range: | 3,487 m | |
| Range notes: | 1.MTOW options:75500 & 77000 kg. 2.MLW option: 66000 kg. 3. MRW option:77400 kg. 4.MZFW option: 62500 kg. | |
| Max passengers: | 0 | |
| Typical passengers: | 180 |
| Category: | Turbofan | |
| Manufacturer: | CFM International | |
| Model/Submodel: | CFM56 5A1 | |
| Thrust: | 111 kN |
| Category: | Turbofan | |
| Manufacturer: | CFM International | |
| Model/Submodel: | CFM56 5A3 | |
| Thrust: | 118 kN |
| Category: | Turbofan | |
| Manufacturer: | IAE International Aero Engines | |
| Model/Submodel: | V2500 A1 | |
| Thrust: | 111 kN |
| Category: | Turbofan | |
| Manufacturer: | IAE International Aero Engines | |
| Model/Submodel: | V2527 A5 | |
| Thrust: | 110 kN |
| Category: | Turbofan | |
| Manufacturer: | IAE International Aero Engines | |
| Model/Submodel: | V2527E A5 | |
| Thrust: | 110 kN |