McDonnell-Douglas MD-11 vs. Airbus A380-800F

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McDonnell-Douglas MD-11 versus Airbus A380-800F
61.20 m 200 ft 10 in length 72.73 m 238 ft 7 in
17.6 m 57 ft 9 in height 24.09 m 79 ft
51.6 m 169 ft 4 in wingspan 79.75 m 261 ft 8 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 4 x Engine Alliance GP7200 turbofan engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons)
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 280,000 to 320,000 pounds
285,990 kg 630,400 lb MTOW 590,000 kg 1,300,733 lb
13,231 km 7,147 nm range 14,800 km 7,992 nm
961 km/h 597 mph cruise speed 903 km/h 561 mph
Max 410 passengers capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.