Airbus A220-100 vs. Lockheed Martin C-130J Super Hercules

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Airbus A220-100 versus Lockheed Martin C-130J Super Hercules
35.0 m 114 ft 10 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 Turbofans (wing mounted) 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
63,100 kg 139,100 lb MTOW 76,610 kg 168,900 lb
6,390 km 3,451 nm range 4,600 km 2,485 nm
871 km/h 541 mph cruise speed 660 km/h 410 mph
Typical seating 2-class 100-120 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.