Airbus A321LR vs. lockheed C-130 hercules

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Airbus A321LR versus lockheed C-130 hercules
44.51 m 146 ft 0 in length 29.79 m 97 ft 9 in
11.76 m 38 ft 7 in height 11.66 m 38 ft 3 in
35.8 m 117 ft 5 in wingspan 40.41 m 132 ft 7 in
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 4 x Allison T56-A-15 turboprop engines
Over 33,000 lbs (147 kN) thrust per engine Approximately 4,590 hp per engine
66,000 lbs (294 kN) total thrust Approximately 18,360 hp total
97,000 kg 213,800 lb MTOW 70,307 kg 155,000 lb
7,400 km 4,000 nm range 3,760 km 2,031 nm
832 km/h 517 mph cruise speed 540 km/h 335 mph
180-220 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.