Airbus A220-300 vs. Canadair CL-415

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Airbus A220-300 versus Canadair CL-415
38.7 m 127 ft 0 in length 19.82 m 65 ft 0 in
11.5 m 37 ft 9 in height 8.66 m 28 ft 5 in
35.1 m 115 ft 2 in wingspan 28.6 m 93 ft 1
2 x Pratt & Whitney PurePower PW1500G engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
21,000–23,000 lb thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
42,000–46,000 lb total thrust 4,300 to 4,760 shaft horsepower
70,900 kg 156,300 lb MTOW 19,733 kg 43,525 lb
6,297 km 3,402 nm range 1,600 km 864 nm
Mach 0.82 101,3 km/h cruise speed 290 km/h 180 mph
Typical seating 2-class 120-150 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.