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