Lockheed Martin C-130J Super Hercules vs. Cessna 208 Caravan

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Lockheed Martin C-130J Super Hercules versus Cessna 208 Caravan
34.37 m 112 ft 9 in length 12.67 m 41 ft 7 in
11.86 m 38 ft 11 in height 4.49 m 14 ft 9 in
40.41 m 132 ft 7 in wingspan 15.88 m 52 ft 1 in
4 x Rolls-Royce AE 2100D3 turboprop engines engines 1 x Pratt & Whitney Canada PT6A-114A turboprop engine
Approximately 4,700 hp per engine thrust per engine 675 shaft horsepower (503 kW)
Approximately 18,800 hp total total thrust 675 shaft horsepower (503 kW)
76,610 kg 168,900 lb MTOW 4,740 kg 10,450 lb
4,600 km 2,485 nm range 1,777 km 960 nm
660 km/h 410 mph cruise speed 340 km/h 211 mph
based on configuration capacity Up to 14 passengers or 3,034 kg
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.