Airbus A220-100 vs. Douglas DC-8

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Airbus A220-100 versus Douglas DC-8
35.0 m 114 ft 10 in length 57.10 m 187 ft 4 in
11.5 m 37 ft 9 in height 16.84 m 55 ft 3 in
35.1 m 115 ft 2 in wingspan 45.24 m 148 ft 5 in
2 Turbofans (wing mounted) engines 4 x Pratt & Whitney JT3D turbofan engines
21,000–23,000 lb thrust per engine Approximately 17,000 lbf per engine
42,000–46,000 lb total thrust Approximately 68,000 lbf total
63,100 kg 139,100 lb MTOW 158,760 kg 350,000 lb
6,390 km 3,451 nm range 11,918 km 6,437 nm
871 km/h 541 mph cruise speed 900 km/h 559 mph
Typical seating 2-class 100-120 capacity Up to 259 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.