Airbus A321XLR vs. Canadair CL-415

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Airbus A321XLR 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
CFM LEAP-1A and P&W PW1100G engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
33,000 lbs (147 kN) thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
66,000 lbs (294 kN) total thrust 4,300 to 4,760 shaft horsepower
101,000 kg 222,700 lb MTOW 19,733 kg 43,525 lb
4,700 nmi 8,704 km range 1,600 km 864 nm
963km/h 598mph cruise speed 290 km/h 180 mph
180-220 seats (typical 2-class seating) 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.