Bombardier CRJ1000 vs. Canadair CL-415

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Bombardier CRJ1000 versus Canadair CL-415
39.1 m 128 ft 5 in length 19.82 m 65 ft 0 in
7.5 m 24 ft 7 in height 8.66 m 28 ft 5 in
26.2 m 86 ft wingspan 28.6 m 93 ft 1
2 GE CF34-8C5A1 turbofans engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
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 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
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 4,300 to 4,760 shaft horsepower
41,640 kg 91,800 lb MTOW 19,733 kg 43,525 lb
3,004 km 1,623 nm range 1,600 km 864 nm
515 mph 829 km/h cruise speed 290 km/h 180 mph
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.