Airbus A220-100 vs. lockheed C-130 hercules

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Airbus A220-100 versus lockheed C-130 hercules
35.0 m 114 ft 10 in length 29.79 m 97 ft 9 in
11.5 m 37 ft 9 in height 11.66 m 38 ft 3 in
35.1 m 115 ft 2 in wingspan 40.41 m 132 ft 7 in
2 Turbofans (wing mounted) engines 4 x Allison T56-A-15 turboprop engines
21,000–23,000 lb thrust per engine Approximately 4,590 hp per engine
42,000–46,000 lb total thrust Approximately 18,360 hp total
63,100 kg 139,100 lb MTOW 70,307 kg 155,000 lb
6,390 km 3,451 nm range 3,760 km 2,031 nm
871 km/h 541 mph cruise speed 540 km/h 335 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.