Airbus A340-500 vs. Canadair CL-415

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Airbus A340-500 versus Canadair CL-415
67.93 m 222 ft 10 in length 19.82 m 65 ft 0 in
17.53 m 57 ft 6 in height 8.66 m 28 ft 5 in
63.45 m 208 ft 2 in wingspan 28.6 m 93 ft 1
4 Rolls-Royce Trent 500 engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
54,000 lbf (240 kN) thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
216,000 lbf (960 kN) total thrust 4,300 to 4,760 shaft horsepower
380,000 kg 837,800 lb MTOW 19,733 kg 43,525 lb
16,670 km 9,000 nm range 1,600 km 864 nm
475 knots 880 km/h cruise speed 290 km/h 180 mph
Typical seating 3-class 270-310 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.