Lockheed Martin C-130J Super Hercules vs. Piper PA-34 Seneca

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Lockheed Martin C-130J Super Hercules versus Piper PA-34 Seneca
34.37 m 112 ft 9 in length 8.71 m 28 ft 7 in
11.86 m 38 ft 11 in height 2.99 m 9 ft 10 in
40.41 m 132 ft 7 in wingspan 11.64 m 38 ft 2 in
4 x Rolls-Royce AE 2100D3 turboprop engines engines 2 x Continental IO-360
Approximately 4,700 hp per engine thrust per engine 220 lbs
Approximately 18,800 hp total total thrust 440 lbs
76,610 kg 168,900 lb MTOW 4,750 lb 2,155 kg
4,600 km 2,485 nm range 980 nm 1,815 km
660 km/h 410 mph cruise speed 165 kts 103 mph
based on configuration capacity 5
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.