Airbus A220-100 vs. Lockheed C-69 Constellation

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Airbus A220-100 versus Lockheed C-69 Constellation
35.0 m 114 ft 10 in length 29.72 m 97 ft 6 in
11.5 m 37 ft 9 in height 6.02 m 19 ft 9 in
35.1 m 115 ft 2 in wingspan 37.49 m 123 ft
2 Turbofans (wing mounted) engines 4 x Wright R-3350 Duplex-Cyclone radial engines
21,000–23,000 lb thrust per engine 2,200 to 3,700 horsepower (1,640 to 2,760 kW)
42,000–46,000 lb total thrust 8,800 to 14,800 horsepower
63,100 kg 139,100 lb MTOW 44,453 kg 98,000 lb
6,390 km 3,451 nm range 5,200 km 2,808 nm
871 km/h 541 mph cruise speed 507 km/h 315 mph
Typical seating 2-class 100-120 capacity Up to 109 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.