Lockheed Martin C-130J Super Hercules vs. Air Tractor AT-802

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Lockheed Martin C-130J Super Hercules versus Air Tractor AT-802
34.37 m 112 ft 9 in length 10.16 m 33 ft 4 in
11.86 m 38 ft 11 in height 3.66 m 12 ft
40.41 m 132 ft 7 in wingspan 18.29 m 60 ft
4 x Rolls-Royce AE 2100D3 turboprop engines engines 1 x Pratt & Whitney Canada PT6A-67F turboprop engine
Approximately 4,700 hp per engine thrust per engine 1,200 to 1,550 shaft horsepower (895 to 1,156 kW)
Approximately 18,800 hp total total thrust 1,200 to 1,550 shaft horsepower (895 to 1,156 kW)
76,610 kg 168,900 lb MTOW 7,257 kg 16,000 lb
4,600 km 2,485 nm range 1,125 km 607 nm
660 km/h 410 mph cruise speed 240 km/h 149 mph
based on configuration capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.