Airbus A220-100 vs. Douglas DC-8-61

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Airbus A220-100 versus Douglas DC-8-61
35.0 m 114 ft 10 in length 57.0 m 187 ft 0 in
11.5 m 37 ft 9 in height 13.1 m 43 ft
35.1 m 115 ft 2 in wingspan 45.24 m 148 ft 5 in
2 Turbofans (wing mounted) engines 4x P&W JT3D-3B Turbofan
21,000–23,000 lb thrust per engine 18,000 pound-force
42,000–46,000 lb total thrust 72,000 pound-force
63,100 kg 139,100 lb MTOW 147,400 kg 325,000 lb
6,390 km 3,451 nm range 3,200 nm 5,926 km
871 km/h 541 mph cruise speed 483 knots 282 mph
Typical seating 2-class 100-120 capacity 180 to 220 passengers in a mixed-class seating
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.