Airbus A319neo vs. North American B-25 Mitchell

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Airbus A319neo versus North American B-25 Mitchell
33.84 m 111 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 x PW 1100G or 2 x CFM LEAP-1A engines 2 x Wright R-2600-92 Twin Cyclone
110kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 1,700 horsepower
220kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 3,400 horsepower
75,500 kg 166,400 lb MTOW 7,484 kg 16,500 lb
6,850 km 3,702 nm range 1,350 mi 1,175 nm
530 mph 853 km/h cruise speed 233 MPH 375 km/h
120-150 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.