Bombardier CRJ900 vs. North American B-25 Mitchell

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Bombardier CRJ900 versus North American B-25 Mitchell
36.2 m 118 ft 11 in length 16.15 m 53 ft 0 in
7.5 m 24 ft 7 in height 5 m 16 ft 4 in
24.9 m 81 ft 8 in wingspan 20.58 m 67 ft 6 in
2 Turbofans (fuselage mounted) engines 2 x Wright R-2600-92 Twin Cyclone
13,360 pounds force thrust per engine 1,700 horsepower
26,720 pounds force total thrust 3,400 horsepower
38,330 kg 84,500 lb MTOW 7,484 kg 16,500 lb
2,871 km 1,550 nm range 1,350 mi 1,175 nm
515 mph 829 km/h cruise speed 233 MPH 375 km/h
Up to 90 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.