Airbus A220-100 vs. McDonnell-Douglas DC-10-30

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Airbus A220-100 versus McDonnell-Douglas DC-10-30
35.0 m 114 ft 10 in length 55.35 m 181 ft 8 in
11.5 m 37 ft 9 in height 17.8 m 58 ft 5 in
35.1 m 115 ft 2 in wingspan 50.39 m 165 ft 4 in
2 Turbofans (wing mounted) engines 3x GE CF6-50C Turbofan
21,000–23,000 lb thrust per engine 54,000 lbf
42,000–46,000 lb total thrust 162,000 lbf
63,100 kg 139,100 lb MTOW 251,744 kg 555,000 lb
6,390 km 3,451 nm range 9,630 km 5,200 nm
871 km/h 541 mph cruise speed 507 knots 939 km/h
Typical seating 2-class 100-120 capacity Up to 380 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.