Airbus A220-300 vs. McDonnell-Douglas DC-10-30

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Airbus A220-300 versus McDonnell-Douglas DC-10-30
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 251,744 kg 555,000 lb
6,297 km 3,402 nm range 9,630 km 5,200 nm
Mach 0.82 101,3 km/h cruise speed 507 knots 939 km/h
Typical seating 2-class 120-150 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.