Airbus A220-100 vs. Douglas C-54 Skymaster

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Airbus A220-100 versus Douglas C-54 Skymaster
35.0 m 114 ft 10 in length 28.60 m 93 ft 10 in
11.5 m 37 ft 9 in height 8.38 m 27 ft 6 in
35.1 m 115 ft 2 in wingspan 35.81 m 117 ft 6 in
2 Turbofans (wing mounted) engines 4 x Pratt & Whitney R-2000 Twin Wasp radial engines
21,000–23,000 lb thrust per engine 1,200 to 1,450 horsepower (895 to 1,080 kW)
42,000–46,000 lb total thrust 4,800 to 5,800 horsepower
63,100 kg 139,100 lb MTOW 29,484 kg 65,000 lb
6,390 km 3,451 nm range 6,500 km 3,510 nm
871 km/h 541 mph cruise speed 340 km/h 211 mph
Typical seating 2-class 100-120 capacity Up to 50 passengers or 28,500 lb cargo
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.