Lockheed Martin C-130J Super Hercules vs. Beechcraft King Air 260

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Lockheed Martin C-130J Super Hercules versus Beechcraft King Air 260
34.37 m 112 ft 9 in length 13.41 m 43 ft 11 in
11.86 m 38 ft 11 in height 4.57 m 15 ft
40.41 m 132 ft 7 in wingspan 17.39 m 57 ft 1 in
4 x Rolls-Royce AE 2100D3 turboprop engines engines 2 x Pratt & Whitney Canada PT6A turboprop
Approximately 4,700 hp per engine thrust per engine 1050 lbs
Approximately 18,800 hp total total thrust 2100 lbs
76,610 kg 168,900 lb MTOW 12,500 lb 5,670 kg
4,600 km 2,485 nm range 1,720 nm 3,185 km
660 km/h 410 mph cruise speed 310 kts 193 mph
based on configuration capacity 9
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.