Airbus A321LR vs. McDonnell-Douglas DC-10-30

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Airbus A321LR 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
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 3x GE CF6-50C Turbofan
Over 33,000 lbs (147 kN) thrust per engine 54,000 lbf
66,000 lbs (294 kN) total thrust 162,000 lbf
97,000 kg 213,800 lb MTOW 251,744 kg 555,000 lb
7,400 km 4,000 nm range 9,630 km 5,200 nm
832 km/h 517 mph cruise speed 507 knots 939 km/h
180-220 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.