Airbus A220-100 vs. Lockheed C-5 Galaxy

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Airbus A220-100 versus Lockheed C-5 Galaxy
35.0 m 114 ft 10 in length 75.31 m 247 ft 2 in
11.5 m 37 ft 9 in height 19.84 m 65 ft 1 in
35.1 m 115 ft 2 in wingspan 67.89 m 222 ft 9 in
2 Turbofans (wing mounted) engines 4 x General Electric TF39 turbofan engines
21,000–23,000 lb thrust per engine 41,000 pounds of thrust (182 kilonewtons)
42,000–46,000 lb total thrust 164,000 pounds
63,100 kg 139,100 lb MTOW 381,018 kg 840,000 lb
6,390 km 3,451 nm range 8,000 km 4,320 nm
871 km/h 541 mph cruise speed 908 km/h 564 mph
Typical seating 2-class 100-120 capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.