Airbus A320neo vs. North American B-25 Mitchell

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Airbus A320neo versus North American B-25 Mitchell
37.57 m 123 ft 3 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 x PW 1100G or 2 x CFM LEAP-1A engines 2 x Wright R-2600-92 Twin Cyclone
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 1,700 horsepower
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 3,400 horsepower
79,000 kg 174,200 lb MTOW 7,484 kg 16,500 lb
6,300 km 3,403 nm range 1,350 mi 1,175 nm
M0.82 101,3 km/h cruise speed 233 MPH 375 km/h
150-180 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.