Airbus A300-600 vs. Boeing F/A-18E/F Super Hornet

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Airbus A300-600 versus Boeing F/A-18E/F Super Hornet
54.10 m 177 ft 6 in length 18.5 m 60 ft 3 in
16.5 m 54 ft 2 in height 4.87 m 16 ft
44.84 m 147 ft 1 in wingspan 13.68 m 44 ft 1
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines Two F414-GE-400 turbofan engines
56,000lb to 61,500lb thrust per engine Up to 17,000 lbs
112,000–123,000 lb total thrust Up to 34,000 lbs
171,700 kg 378,600 lb MTOW 29,937 kg 66,000 lb
7,500 km 4,052 nm range 2,346 km 1,268 nm
897 km/h 557 mph cruise speed 1032 knots 1,911 km/h
210-250 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.