Airbus A319neo vs. Lockheed Martin C-130J Super Hercules

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Airbus A319neo versus Lockheed Martin C-130J Super Hercules
33.84 m 111 ft 0 in length 34.37 m 112 ft 9 in
11.76 m 38 ft 7 in height 11.86 m 38 ft 11 in
35.8 m 117 ft 5 in wingspan 40.41 m 132 ft 7 in
2 x PW 1100G or 2 x CFM LEAP-1A engines 4 x Rolls-Royce AE 2100D3 turboprop engines
110kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine Approximately 4,700 hp per engine
220kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust Approximately 18,800 hp total
75,500 kg 166,400 lb MTOW 76,610 kg 168,900 lb
6,850 km 3,702 nm range 4,600 km 2,485 nm
530 mph 853 km/h cruise speed 660 km/h 410 mph
120-150 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.