Airbus A220-100 vs. McDonnell-Douglas DC-9-30

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Airbus A220-100 versus McDonnell-Douglas DC-9-30
35.0 m 114 ft 10 in length 36.36 m 119 ft 3 in
11.5 m 37 ft 9 in height 8.5 m 27 ft 11 in
35.1 m 115 ft 2 in wingspan 28.44 m 93 ft 4 in
2 Turbofans (wing mounted) engines 2x Pratt & Whitney JT8D
21,000–23,000 lb thrust per engine 15,000 pound-force
42,000–46,000 lb total thrust 30,000 pound-force (2 engines)
63,100 kg 139,100 lb MTOW 54,885 kg 121,000 lb
6,390 km 3,451 nm range 2,632 km 1,422 nm
871 km/h 541 mph cruise speed 898 km/h 558 mph
Typical seating 2-class 100-120 capacity Up to 139 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.