Lockheed Martin C-130J Super Hercules vs. Cessna 172

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Lockheed Martin C-130J Super Hercules versus Cessna 172
34.37 m 112 ft 9 in length 8.28 m 27 ft 2 in
11.86 m 38 ft 11 in height 2.72 m 8 ft 11 in
40.41 m 132 ft 7 in wingspan 11 m 36 ft 1 in
4 x Rolls-Royce AE 2100D3 turboprop engines engines 1 x Lycoming IO-360-L2A flat-4 piston engine
Approximately 4,700 hp per engine thrust per engine 180 to 200 horsepower (134 to 149 kW)
Approximately 18,800 hp total total thrust 180 to 200 horsepower (134 to 149 kW)
76,610 kg 168,900 lb MTOW 1,040 kg 2,293 lb
4,600 km 2,485 nm range 1,056 km 570 nm
660 km/h 410 mph cruise speed 226 km/h 140 mph
based on configuration capacity 4
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.