Airbus A320-200 vs. McDonnell-Douglas MD-11

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Airbus A320-200 versus McDonnell-Douglas MD-11
38.7 m 127 ft 0 in length 61.20 m 200 ft 10 in
17.4 m 57 ft 1 in height 17.6 m 57 ft 9 in
35.8 m 117 ft 5 in wingspan 51.6 m 169 ft 4 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462)
Between 21,000 - 33,000 lbf thrust per engine 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460)
Between 42,000 - 66,000 lbf total thrust 819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460)
77,000 kg 169,800 lb MTOW 285,990 kg 630,400 lb
5,700 km 3,078 nm range 13,231 km 7,147 nm
530 mph 853 km/h cruise speed 961 km/h 597 mph
Typically between 140-180 passengers 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.