Airbus A340-200 vs. Canadair CL-415

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Airbus A340-200 versus Canadair CL-415
59.4 m 194 ft 11 in length 19.82 m 65 ft 0 in
16.8 m 55 ft 1 in height 8.66 m 28 ft 5 in
60.3 m 197 ft 9 in wingspan 28.6 m 93 ft 1
4 x CFM International CFM56-5C4 engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
34,000 lbf thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
136,000 lbf total thrust 4,300 to 4,760 shaft horsepower
275,000 kg 606,300 lb MTOW 19,733 kg 43,525 lb
12,400 km 6,699 nm range 1,600 km 864 nm
880 km/h 547 mph cruise speed 290 km/h 180 mph
Typical seating 3-class 210-250 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.