Airbus A321LR vs. North American B-25 Mitchell

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Airbus A321LR versus North American B-25 Mitchell
44.51 m 146 ft 0 in length 16.15 m 53 ft 0 in
11.76 m 38 ft 7 in height 5 m 16 ft 4 in
35.8 m 117 ft 5 in wingspan 20.58 m 67 ft 6 in
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 2 x Wright R-2600-92 Twin Cyclone
Over 33,000 lbs (147 kN) thrust per engine 1,700 horsepower
66,000 lbs (294 kN) total thrust 3,400 horsepower
97,000 kg 213,800 lb MTOW 7,484 kg 16,500 lb
7,400 km 4,000 nm range 1,350 mi 1,175 nm
832 km/h 517 mph cruise speed 233 MPH 375 km/h
180-220 passengers capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.