Mac Donnell Douglas DC-9-10
Entry into service | 1965 |
Dimensions | Length : 31.82 m |
Wing span : 27.25 m | |
Height : 8.38 m | |
Weights | Maximum take off weight : 35,245 kg |
Maximum landing weight : 33,565 kg | |
Operating empty weight : 20,550 kg | |
Maximum payload : 8,188 kg | |
Powerplant | 2 x 12,250 lb (5,556 kg) Pratt & Whitney JT8D-5. |
Fuel capacity | 10,546 l |
Performance | Maximum cruise speed : 487 kt - 903 km/h |
Maximum cruising altitude : 35,000 ft - 10,600 m | |
T-O distance : 1,615 m | |
Landing field length : 1,411 m | |
Design range : 2,110 km/50 pax. | |
Accommodations | 1-class : 80 |
2-class : - | |
3-class : - |