Airbus A220-100 vs. McDonnell-Douglas MD-11

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Airbus A220-100 versus McDonnell-Douglas MD-11
35.0 m 114 ft 10 in length 61.20 m 200 ft 10 in
11.5 m 37 ft 9 in height 17.6 m 57 ft 9 in
35.1 m 115 ft 2 in wingspan 51.6 m 169 ft 4 in
2 Turbofans (wing mounted) engines 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462)
21,000–23,000 lb thrust per engine 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460)
42,000–46,000 lb total thrust 819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460)
63,100 kg 139,100 lb MTOW 285,990 kg 630,400 lb
6,390 km 3,451 nm range 13,231 km 7,147 nm
871 km/h 541 mph cruise speed 961 km/h 597 mph
Typical seating 2-class 100-120 capacity Max 410 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.