Airbus A321XLR vs. Lockheed Martin C-130J Super Hercules

versus
... or view the full comparison list here.
Airbus A321XLR versus Lockheed Martin C-130J Super Hercules
44.51 m 146 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
CFM LEAP-1A and P&W PW1100G engines 4 x Rolls-Royce AE 2100D3 turboprop engines
33,000 lbs (147 kN) thrust per engine Approximately 4,700 hp per engine
66,000 lbs (294 kN) total thrust Approximately 18,800 hp total
101,000 kg 222,700 lb MTOW 76,610 kg 168,900 lb
4,700 nmi 8,704 km range 4,600 km 2,485 nm
963km/h 598mph cruise speed 660 km/h 410 mph
180-220 seats (typical 2-class seating) 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.