Airbus A300-600F vs. Canadair CL-415

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Airbus A300-600F versus Canadair CL-415
54.08 m 177 ft 5 in length 19.82 m 65 ft 0 in
17.05 m 55 ft 11 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 General Electric CF6-80C2A5 turbofan engines engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
Approximately 59,000 lbf per engine thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
Approximately 118,000 lbf total total thrust 4,300 to 4,760 shaft horsepower
170,000 kg 374,786 lb MTOW 19,733 kg 43,525 lb
4,830 km 2,608 nm range 1,600 km 864 nm
860 km/h 534 mph cruise speed 290 km/h 180 mph
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.