Airbus A321-200 vs. McDonnell-Douglas DC-9-30
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Airbus A321-200 |
versus |
McDonnell-Douglas DC-9-30 |
44.51 m |
146 ft 0 in |
length |
36.36 m |
119 ft 3 in |
11.76 m |
38 ft 7 in |
height |
8.5 m |
27 ft 11 in |
35.8 m |
117 ft 5 in |
wingspan |
28.44 m |
93 ft 4 in |
2 GE CFM56-5B3 |
engines |
2x Pratt & Whitney JT8D |
31,600 lbs |
thrust per engine |
15,000 pound-force |
63,200 lbs |
total thrust |
30,000 pound-force (2 engines) |
89,000 kg |
196,200 lb |
MTOW |
54,885 kg |
121,000 lb |
4,000 nmi |
7,408 km |
range |
2,632 km |
1,422 nm |
871 km/h |
541 mph |
cruise speed |
898 km/h |
558 mph |
185 to 220 |
capacity |
Up to 139 passengers |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.