Airbus A310-300 vs. Boeing F/A-18E/F Super Hornet

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Airbus A310-300 versus Boeing F/A-18E/F Super Hornet
46.66 m 153 ft 1 in length 18.5 m 60 ft 3 in
15.8 m 51 ft 10 in height 4.87 m 16 ft
43.9 m 144 ft wingspan 13.68 m 44 ft 1
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines Two F414-GE-400 turbofan engines
52,000 lb thrust per engine Up to 17,000 lbs
104,000 lb total thrust Up to 34,000 lbs
148,768 kg 328,000 lb MTOW 29,937 kg 66,000 lb
8,050 km 4,348 nm range 2,346 km 1,268 nm
482 knots 279 mph cruise speed 1032 knots 1,911 km/h
190-230 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.