Mac Donnell Douglas DC-9-20
| Entry into service | 1969 |
| Dimensions | Length : 31.82 m |
| Wing span : 28.47 m | |
| Height : 8.38 m | |
| Weights | Maximum take off weight : 44,450 kg |
| Maximum landing weight : 42,365 kg | |
| Operating empty weight : 22,620 kg | |
| Maximum payload : 9,925 kg | |
| Powerplant | 2 x 14,500 lb (6,575 kg) Pratt & Whitney JT8D-9. |
| Fuel capacity | 13,925 l |
| Performance | Maximum cruise speed : 487 kt - 903 km/h |
| Maximum cruising altitude : 35,000 ft - 10,600 m | |
| T-O distance : 1,750 m | |
| Landing field length : 1,460 m | |
| Design range : 2,970 km/50 pax. | |
| Accommodations | 1-class : 90 |
| 2-class : 68 | |
| 3-class : 56 |