Mac Donnell Douglas DC-9-30
| Entry into service | 1967 | |
| Dimensions | Length : 36.37 m | |
| Wing span : 28.47 m | ||
| Height : 8.38 m | ||
| Weights | Maximum take off weight : | 49,895 kg |
| Option : 54,940 kg | ||
| Maximum landing weight : 45,814 kg | ||
| Operating empty weight : 25,400 kg | ||
| Maximum payload : 16,330 kg | ||
| Powerplant | 2 x 14,000 - 15,500lb (6,365 - 7,045 kg) Pratt & Whitney JT8D-7/9/11 or 15. | |
| Fuel capacity | 13,925 l | |
| Performance | Maximum cruise speed : 503 kt - 932 km/h | |
| Maximum cruising altitude : 35,000 ft - 10,600 m | ||
| T-O distance : 1,777 m | ||
| Landing field length : 1,317 m | ||
| Design range : 2,220 km/12,000 kg payload. | ||
| Accommodations | 1-class : 115 | |
| 2-class : 105 | ||
| 3-class : - | ||