Airbus A220-100 vs. Canadair CL-415

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Airbus A220-100 versus Canadair CL-415
35.0 m 114 ft 10 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 Turbofans (wing mounted) 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
63,100 kg 139,100 lb MTOW 19,733 kg 43,525 lb
6,390 km 3,451 nm range 1,600 km 864 nm
871 km/h 541 mph cruise speed 290 km/h 180 mph
Typical seating 2-class 100-120 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.