Airbus A220-300 vs. North American B-25 Mitchell

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Airbus A220-300 versus North American B-25 Mitchell
38.7 m 127 ft 0 in length 16.15 m 53 ft 0 in
11.5 m 37 ft 9 in height 5 m 16 ft 4 in
35.1 m 115 ft 2 in wingspan 20.58 m 67 ft 6 in
2 x Pratt & Whitney PurePower PW1500G engines 2 x Wright R-2600-92 Twin Cyclone
21,000–23,000 lb thrust per engine 1,700 horsepower
42,000–46,000 lb total thrust 3,400 horsepower
70,900 kg 156,300 lb MTOW 7,484 kg 16,500 lb
6,297 km 3,402 nm range 1,350 mi 1,175 nm
Mach 0.82 101,3 km/h cruise speed 233 MPH 375 km/h
Typical seating 2-class 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.