Airbus A330-300 vs. Canadair CL-415

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Airbus A330-300 versus Canadair CL-415
63.66 m 208 ft 9 in length 19.82 m 65 ft 0 in
16.79 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
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
Depends on the engine type total thrust 4,300 to 4,760 shaft horsepower
242,000 kg 533,600 lb MTOW 19,733 kg 43,525 lb
11,750 km 6,346 nm range 1,600 km 864 nm
900 km/h 559 mph cruise speed 290 km/h 180 mph
250-290 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.