Airbus A340-600 vs. McDonnell-Douglas MD-11

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Airbus A340-600 versus McDonnell-Douglas MD-11
75.36 m 247 ft 3 in length 61.20 m 200 ft 10 in
17.93 m 58 ft 10 in height 17.6 m 57 ft 9 in
63.45 m 208 ft 2 in wingspan 51.6 m 169 ft 4 in
4 x Rolls-Royce Trent 556 engines 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462)
56,000 lbs thrust per engine 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460)
224,000 lbs total thrust 819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460)
380,000 kg 837,800 lb MTOW 285,990 kg 630,400 lb
14,450 km 7,804 nm range 13,231 km 7,147 nm
890 km/h 553 mph cruise speed 961 km/h 597 mph
320-370 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.