Airbus A321-200 vs. North American B-25 Mitchell

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Airbus A321-200 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
2 GE CFM56-5B3 engines 2 x Wright R-2600-92 Twin Cyclone
31,600 lbs thrust per engine 1,700 horsepower
63,200 lbs total thrust 3,400 horsepower
89,000 kg 196,200 lb MTOW 7,484 kg 16,500 lb
4,000 nmi 7,408 km range 1,350 mi 1,175 nm
871 km/h 541 mph cruise speed 233 MPH 375 km/h
185 to 220 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.