Airbus A220-300 vs. Lockheed Martin C-130J Super Hercules

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Airbus A220-300 versus Lockheed Martin C-130J Super Hercules
38.7 m 127 ft 0 in length 34.37 m 112 ft 9 in
11.5 m 37 ft 9 in height 11.86 m 38 ft 11 in
35.1 m 115 ft 2 in wingspan 40.41 m 132 ft 7 in
2 x Pratt & Whitney PurePower PW1500G engines 4 x Rolls-Royce AE 2100D3 turboprop engines
21,000–23,000 lb thrust per engine Approximately 4,700 hp per engine
42,000–46,000 lb total thrust Approximately 18,800 hp total
70,900 kg 156,300 lb MTOW 76,610 kg 168,900 lb
6,297 km 3,402 nm range 4,600 km 2,485 nm
Mach 0.82 101,3 km/h cruise speed 660 km/h 410 mph
Typical seating 2-class 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.