Airbus A321XLR vs. North American B-25 Mitchell

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Airbus A321XLR 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 LEAP-1A and P&W PW1100G engines 2 x Wright R-2600-92 Twin Cyclone
33,000 lbs (147 kN) thrust per engine 1,700 horsepower
66,000 lbs (294 kN) total thrust 3,400 horsepower
101,000 kg 222,700 lb MTOW 7,484 kg 16,500 lb
4,700 nmi 8,704 km range 1,350 mi 1,175 nm
963km/h 598mph cruise speed 233 MPH 375 km/h
180-220 seats (typical 2-class seating) 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.