Lockheed Martin C-130J Super Hercules vs. Aero Commander 680

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Lockheed Martin C-130J Super Hercules versus Aero Commander 680
34.37 m 112 ft 9 in length 11.38 m 37 ft 4 in
11.86 m 38 ft 11 in height 3.6 m 11 ft 10 in
40.41 m 132 ft 7 in wingspan 15.02 m 49 ft 3 in
4 x Rolls-Royce AE 2100D3 turboprop engines engines 2 x Lycoming TIO-540
Approximately 4,700 hp per engine thrust per engine 380 lbs
Approximately 18,800 hp total total thrust 760 lbs
76,610 kg 168,900 lb MTOW 7,500 lb 3,402 kg
4,600 km 2,485 nm range 1,500 nm 2,778 km
660 km/h 410 mph cruise speed 218 kts 135 mph
based on configuration capacity Up to 6 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.