Airbus A300-600 vs. Boeing 787-8

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Airbus A300-600 versus Boeing 787-8
54.10 m 177 ft 6 in length 57.0 m 187 ft 0 in
16.5 m 54 ft 2 in height 17 m 55 ft 9 in
44.84 m 147 ft 1 in wingspan 60 m 196 ft 1
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines GEnx-1B / Trent 1000
56,000lb to 61,500lb thrust per engine 265.1 kN (59600 lbf) for Trent 1000-E, 321.6 kN (72300 lbf) for GEnx-1B70
112,000–123,000 lb total thrust 2 * 265.1 kN (59600 lbf) for Trent 1000-E, 2 * 321.6 kN (72300 lbf) for GEnx-1B70
171,700 kg 378,600 lb MTOW 227,930 kg 502,500 lb
7,500 km 4,052 nm range 13,530 km 7,305 nmi
897 km/h 557 mph cruise speed 652 mph 1,050 kph
210-250 passengers capacity 248
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.