Lockheed Martin C-130J Super Hercules vs. de Havilland Canada DHC-6 Twin Otter

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Lockheed Martin C-130J Super Hercules versus de Havilland Canada DHC-6 Twin Otter
34.37 m 112 ft 9 in length 15.32 m 50 ft 3 in
11.86 m 38 ft 11 in height 5.94 m 19 ft 6 in
40.41 m 132 ft 7 in wingspan 19.81 m 65 ft
4 x Rolls-Royce AE 2100D3 turboprop engines engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
Approximately 4,700 hp per engine thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
Approximately 18,800 hp total total thrust 1100 to 1500 shaft horsepower
76,610 kg 168,900 lb MTOW 5,670 kg 12,500 lb
4,600 km 2,485 nm range 1,389 km 750 nm
660 km/h 410 mph cruise speed 280 km/h 174 mph
based on configuration capacity 19 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.