Airbus A321-200 vs. Canadair CL-415

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Airbus A321-200 versus Canadair CL-415
44.51 m 146 ft 0 in length 19.82 m 65 ft 0 in
11.76 m 38 ft 7 in height 8.66 m 28 ft 5 in
35.8 m 117 ft 5 in wingspan 28.6 m 93 ft 1
2 GE CFM56-5B3 engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
31,600 lbs thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
63,200 lbs total thrust 4,300 to 4,760 shaft horsepower
89,000 kg 196,200 lb MTOW 19,733 kg 43,525 lb
4,000 nmi 7,408 km range 1,600 km 864 nm
871 km/h 541 mph cruise speed 290 km/h 180 mph
185 to 220 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.