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
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.