Airbus A340-200 vs. Lockheed Martin C-130J Super Hercules

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Airbus A340-200 versus Lockheed Martin C-130J Super Hercules
59.4 m 194 ft 11 in length 34.37 m 112 ft 9 in
16.8 m 55 ft 1 in height 11.86 m 38 ft 11 in
60.3 m 197 ft 9 in wingspan 40.41 m 132 ft 7 in
4 x CFM International CFM56-5C4 engines 4 x Rolls-Royce AE 2100D3 turboprop engines
34,000 lbf thrust per engine Approximately 4,700 hp per engine
136,000 lbf total thrust Approximately 18,800 hp total
275,000 kg 606,300 lb MTOW 76,610 kg 168,900 lb
12,400 km 6,699 nm range 4,600 km 2,485 nm
880 km/h 547 mph cruise speed 660 km/h 410 mph
Typical seating 3-class 210-250 capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.