Airbus A220-300 vs. lockheed C-130 hercules

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Airbus A220-300 versus lockheed C-130 hercules
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 70,307 kg 155,000 lb
6,297 km 3,402 nm range 3,760 km 2,031 nm
Mach 0.82 101,3 km/h cruise speed 540 km/h 335 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.