Airbus A340-200 vs. McDonnell-Douglas DC-9-30
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Airbus A340-200 |
versus |
McDonnell-Douglas DC-9-30 |
59.4 m |
194 ft 11 in |
length |
36.36 m |
119 ft 3 in |
16.8 m |
55 ft 1 in |
height |
8.5 m |
27 ft 11 in |
60.3 m |
197 ft 9 in |
wingspan |
28.44 m |
93 ft 4 in |
4 x CFM International CFM56-5C4 |
engines |
2x Pratt & Whitney JT8D |
34,000 lbf |
thrust per engine |
15,000 pound-force |
136,000 lbf |
total thrust |
30,000 pound-force (2 engines) |
275,000 kg |
606,300 lb |
MTOW |
54,885 kg |
121,000 lb |
12,400 km |
6,699 nm |
range |
2,632 km |
1,422 nm |
880 km/h |
547 mph |
cruise speed |
898 km/h |
558 mph |
Typical seating 3-class 210-250 |
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.