Mac Donnell Douglas DC-9-15
Entry into service 1966
Dimensions Length : 31.82 m
Wing span : 27.25 m
Height : 8.38 m
Weights Maximum take off weight : 41,140 kg
Maximum landing weight : 37,060 kg
Operating empty weight : 21,660 kg
Maximum payload : 9,696 kg
Powerplant 2 x 14,000 lb (6,350 kg) Pratt & Whitney JT8D-5.
Fuel capacity 14,000 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 : -