Airbus A318 vs. North American B-25 Mitchell

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Airbus A318 versus North American B-25 Mitchell
31.44 m 103 ft 2 in length 16.15 m 53 ft 0 in
12.56 m 41 ft 3 in height 5 m 16 ft 4 in
34.1 m 111 ft 11 in wingspan 20.58 m 67 ft 6 in
2x CFM56-5B or 2x PW6000 engines 2 x Wright R-2600-92 Twin Cyclone
23,300 lb thrust per engine 1,700 horsepower
46,600 lb total thrust 3,400 horsepower
59,000 kg 130,000 lb MTOW 7,484 kg 16,500 lb
5,750 km 3,106 nm range 1,350 mi 1,175 nm
963km/h 598mph cruise speed 233 MPH 375 km/h
107 to 132 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.