Airbus A320-200 vs. North American B-25 Mitchell

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Airbus A320-200 versus North American B-25 Mitchell
38.7 m 127 ft 0 in length 16.15 m 53 ft 0 in
17.4 m 57 ft 1 in height 5 m 16 ft 4 in
35.8 m 117 ft 5 in wingspan 20.58 m 67 ft 6 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2 x Wright R-2600-92 Twin Cyclone
Between 21,000 - 33,000 lbf thrust per engine 1,700 horsepower
Between 42,000 - 66,000 lbf total thrust 3,400 horsepower
77,000 kg 169,800 lb MTOW 7,484 kg 16,500 lb
5,700 km 3,078 nm range 1,350 mi 1,175 nm
530 mph 853 km/h cruise speed 233 MPH 375 km/h
Typically between 140-180 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.