Airbus A318 vs. Lockheed Martin C-130J Super Hercules

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Airbus A318 versus Lockheed Martin C-130J Super Hercules
31.44 m 103 ft 2 in length 34.37 m 112 ft 9 in
12.56 m 41 ft 3 in height 11.86 m 38 ft 11 in
34.1 m 111 ft 11 in wingspan 40.41 m 132 ft 7 in
2x CFM56-5B or 2x PW6000 engines 4 x Rolls-Royce AE 2100D3 turboprop engines
23,300 lb thrust per engine Approximately 4,700 hp per engine
46,600 lb total thrust Approximately 18,800 hp total
59,000 kg 130,000 lb MTOW 76,610 kg 168,900 lb
5,750 km 3,106 nm range 4,600 km 2,485 nm
963km/h 598mph cruise speed 660 km/h 410 mph
107 to 132 passengers 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.