Airbus A320-200 vs. Canadair CL-415

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Airbus A320-200 versus Canadair CL-415
38.7 m 127 ft 0 in length 19.82 m 65 ft 0 in
17.4 m 57 ft 1 in height 8.66 m 28 ft 5 in
35.8 m 117 ft 5 in wingspan 28.6 m 93 ft 1
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
Between 21,000 - 33,000 lbf thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
Between 42,000 - 66,000 lbf total thrust 4,300 to 4,760 shaft horsepower
77,000 kg 169,800 lb MTOW 19,733 kg 43,525 lb
5,700 km 3,078 nm range 1,600 km 864 nm
530 mph 853 km/h cruise speed 290 km/h 180 mph
Typically between 140-180 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.