Lockheed Martin C-130J Super Hercules vs. Canadair CL-415

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Lockheed Martin C-130J Super Hercules versus Canadair CL-415
34.37 m 112 ft 9 in length 19.82 m 65 ft 0 in
11.86 m 38 ft 11 in height 8.66 m 28 ft 5 in
40.41 m 132 ft 7 in wingspan 28.6 m 93 ft 1
4 x Rolls-Royce AE 2100D3 turboprop engines engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
Approximately 4,700 hp per engine thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
Approximately 18,800 hp total total thrust 4,300 to 4,760 shaft horsepower
76,610 kg 168,900 lb MTOW 19,733 kg 43,525 lb
4,600 km 2,485 nm range 1,600 km 864 nm
660 km/h 410 mph cruise speed 290 km/h 180 mph
based on configuration 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.