Airbus A321-200 vs. McDonnell-Douglas DC-10-30

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Airbus A321-200 versus McDonnell-Douglas DC-10-30
44.51 m 146 ft 0 in length 55.35 m 181 ft 8 in
11.76 m 38 ft 7 in height 17.8 m 58 ft 5 in
35.8 m 117 ft 5 in wingspan 50.39 m 165 ft 4 in
2 GE CFM56-5B3 engines 3x GE CF6-50C Turbofan
31,600 lbs thrust per engine 54,000 lbf
63,200 lbs total thrust 162,000 lbf
89,000 kg 196,200 lb MTOW 251,744 kg 555,000 lb
4,000 nmi 7,408 km range 9,630 km 5,200 nm
871 km/h 541 mph cruise speed 507 knots 939 km/h
185 to 220 capacity Up to 380 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.