Airbus A320-200 vs. McDonnell-Douglas DC-10-30

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Airbus A320-200 versus McDonnell-Douglas DC-10-30
38.7 m 127 ft 0 in length 55.35 m 181 ft 8 in
17.4 m 57 ft 1 in height 17.8 m 58 ft 5 in
35.8 m 117 ft 5 in wingspan 50.39 m 165 ft 4 in
Choice between Pratt & Whitney GTFâ„¢ and the LEAP-1A from CFM International engines 3x GE CF6-50C Turbofan
Between 21,000 - 33,000 lbf thrust per engine 54,000 lbf
Between 42,000 - 66,000 lbf total thrust 162,000 lbf
77,000 kg 169,800 lb MTOW 251,744 kg 555,000 lb
5,700 km 3,078 nm range 9,630 km 5,200 nm
530 mph 853 km/h cruise speed 507 knots 939 km/h
Typically between 140-180 passengers 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.