Mac Donnell Douglas DC-9-50
Entry into service | 1975+ |
Dimensions | Length : 40.7 m |
Wing span : 28.47 m | |
Height : 8.38 m | |
Weights | Maximum take off weight : 54,420 kg |
Maximum landing weight : 49,885 kg | |
Operating empty weight : 29,300 kg | |
Maximum payload : 15,370 kg | |
Powerplant | 2 x 15,500 - 16,200lb (7,045 - 7,364 kg) Pratt & Whitney JT8D-15/17. |
Fuel capacity | 16,120 l |
Performance | Maximum cruise speed : 501 kt - 928 km/h |
Maximum cruising altitude : 35,000 ft - 10,600 m | |
T-O distance : 2,362 m | |
Landing field length : 1,439 m | |
Design range : 1,850 km/14,000 kg payload. | |
Accommodations | 1-class : 139 |
2-class : 125 | |
3-class : - |