Airbus A340-500 vs. Lockheed Martin C-130J Super Hercules

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Airbus A340-500 versus Lockheed Martin C-130J Super Hercules
67.93 m 222 ft 10 in length 34.37 m 112 ft 9 in
17.53 m 57 ft 6 in height 11.86 m 38 ft 11 in
63.45 m 208 ft 2 in wingspan 40.41 m 132 ft 7 in
4 Rolls-Royce Trent 500 engines 4 x Rolls-Royce AE 2100D3 turboprop engines
54,000 lbf (240 kN) thrust per engine Approximately 4,700 hp per engine
216,000 lbf (960 kN) total thrust Approximately 18,800 hp total
380,000 kg 837,800 lb MTOW 76,610 kg 168,900 lb
16,670 km 9,000 nm range 4,600 km 2,485 nm
475 knots 880 km/h cruise speed 660 km/h 410 mph
Typical seating 3-class 270-310 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.