Airbus A340-500 vs. McDonnell-Douglas MD-11

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Airbus A340-500 versus McDonnell-Douglas MD-11
67.93 m 222 ft 10 in length 61.20 m 200 ft 10 in
17.53 m 57 ft 6 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 Rolls-Royce Trent 500 engines 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462)
54,000 lbf (240 kN) thrust per engine 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460)
216,000 lbf (960 kN) 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
16,670 km 9,000 nm range 13,231 km 7,147 nm
475 knots 880 km/h cruise speed 961 km/h 597 mph
Typical seating 3-class 270-310 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.