Airbus A320-200 vs. McDonnell-Douglas DC-9-30

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Airbus A320-200 versus McDonnell-Douglas DC-9-30
38.7 m 127 ft 0 in length 36.36 m 119 ft 3 in
17.4 m 57 ft 1 in height 8.5 m 27 ft 11 in
35.8 m 117 ft 5 in wingspan 28.44 m 93 ft 4 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2x Pratt & Whitney JT8D
Between 21,000 - 33,000 lbf thrust per engine 15,000 pound-force
Between 42,000 - 66,000 lbf total thrust 30,000 pound-force (2 engines)
77,000 kg 169,800 lb MTOW 54,885 kg 121,000 lb
5,700 km 3,078 nm range 2,632 km 1,422 nm
530 mph 853 km/h cruise speed 898 km/h 558 mph
Typically between 140-180 passengers 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.