Airbus A220-100 vs. North American B-25 Mitchell

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Airbus A220-100 versus North American B-25 Mitchell
35.0 m 114 ft 10 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 Turbofans (wing mounted) 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
63,100 kg 139,100 lb MTOW 7,484 kg 16,500 lb
6,390 km 3,451 nm range 1,350 mi 1,175 nm
871 km/h 541 mph cruise speed 233 MPH 375 km/h
Typical seating 2-class 100-120 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.