Airbus A340-200 vs. McDonnell-Douglas MD-11

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Airbus A340-200 versus McDonnell-Douglas MD-11
59.4 m 194 ft 11 in length 61.20 m 200 ft 10 in
16.8 m 55 ft 1 in height 17.6 m 57 ft 9 in
60.3 m 197 ft 9 in wingspan 51.6 m 169 ft 4 in
4 x CFM International CFM56-5C4 engines 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462)
34,000 lbf thrust per engine 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460)
136,000 lbf total thrust 819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460)
275,000 kg 606,300 lb MTOW 285,990 kg 630,400 lb
12,400 km 6,699 nm range 13,231 km 7,147 nm
880 km/h 547 mph cruise speed 961 km/h 597 mph
Typical seating 3-class 210-250 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.