McDonnell-Douglas MD-11 vs. Boeing F/A-18E/F Super Hornet

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McDonnell-Douglas MD-11 versus Boeing F/A-18E/F Super Hornet
61.20 m 200 ft 10 in length 18.5 m 60 ft 3 in
17.6 m 57 ft 9 in height 4.87 m 16 ft
51.6 m 169 ft 4 in wingspan 13.68 m 44 ft 1
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines Two F414-GE-400 turbofan engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine Up to 17,000 lbs
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust Up to 34,000 lbs
285,990 kg 630,400 lb MTOW 29,937 kg 66,000 lb
13,231 km 7,147 nm range 2,346 km 1,268 nm
961 km/h 597 mph cruise speed 1032 knots 1,911 km/h
Max 410 passengers capacity Overall capability across all eleven hardpoints is 17,750lbs of external stores
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.