lockheed C-130 hercules vs. Piper PA-34 Seneca

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lockheed C-130 hercules versus Piper PA-34 Seneca
29.79 m 97 ft 9 in length 8.71 m 28 ft 7 in
11.66 m 38 ft 3 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 Allison T56-A-15 turboprop engines engines 2 x Continental IO-360
Approximately 4,590 hp per engine thrust per engine 220 lbs
Approximately 18,360 hp total total thrust 440 lbs
70,307 kg 155,000 lb MTOW 4,750 lb 2,155 kg
3,760 km 2,031 nm range 980 nm 1,815 km
540 km/h 335 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.