Airbus A300-600 vs. Canadair CL-415

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Airbus A300-600 versus Canadair CL-415
54.10 m 177 ft 6 in length 19.82 m 65 ft 0 in
16.5 m 54 ft 2 in height 8.66 m 28 ft 5 in
44.84 m 147 ft 1 in wingspan 28.6 m 93 ft 1
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
56,000lb to 61,500lb thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
112,000–123,000 lb total thrust 4,300 to 4,760 shaft horsepower
171,700 kg 378,600 lb MTOW 19,733 kg 43,525 lb
7,500 km 4,052 nm range 1,600 km 864 nm
897 km/h 557 mph cruise speed 290 km/h 180 mph
210-250 passengers 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.