Lockheed Martin C-130J Super Hercules vs. Beechcraft T-6 Texan II

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Lockheed Martin C-130J Super Hercules versus Beechcraft T-6 Texan II
34.37 m 112 ft 9 in length 10.18 m 33 ft 4 in
11.86 m 38 ft 11 in height 3.29 m 10 ft 10 in
40.41 m 132 ft 7 in wingspan 10.21 m 33 ft 6 in
4 x Rolls-Royce AE 2100D3 turboprop engines engines 1 x Pratt & Whitney Canada PT6A-68
Approximately 4,700 hp per engine thrust per engine 1100 lbs
Approximately 18,800 hp total total thrust 1100 lbs
76,610 kg 168,900 lb MTOW 6,250 lb 2,835 kg
4,600 km 2,485 nm range 900 nm 1,667 km
660 km/h 410 mph cruise speed 320 kts 199 mph
based on configuration capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.