Mac Donnell Douglas DC-9-40
| Entry into service | 1968 |
| Dimensions | Length : 38.28 m |
| Wing span : 28.47 m | |
| Height : 8.38 m | |
| Weights | Maximum take off weight : 51,710 kg |
| Maximum landing weight : 46,625 kg | |
| Operating empty weight : 25,461 kg | |
| Maximum payload : 15,510 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 : 2,462 m | |
| Landing field length : 1,456 m | |
| Design range : 2,710 km/- kg payload. | |
| Accommodations | 1-class : 125 |
| 2-class : - | |
| 3-class : - |