Bombardier CRJ1000 vs. North American B-25 Mitchell

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Bombardier CRJ1000 versus North American B-25 Mitchell
39.1 m 128 ft 5 in length 16.15 m 53 ft 0 in
7.5 m 24 ft 7 in height 5 m 16 ft 4 in
26.2 m 86 ft wingspan 20.58 m 67 ft 6 in
2 GE CF34-8C5A1 turbofans engines 2 x Wright R-2600-92 Twin Cyclone
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve thrust per engine 1,700 horsepower
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust 3,400 horsepower
41,640 kg 91,800 lb MTOW 7,484 kg 16,500 lb
3,004 km 1,623 nm range 1,350 mi 1,175 nm
515 mph 829 km/h cruise speed 233 MPH 375 km/h
100 (common) 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.