Airbus A300-600 vs. Airbus A310-300

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Airbus A300-600 versus Airbus A310-300
54.10 m 177 ft 6 in length 46.66 m 153 ft 1 in
16.5 m 54 ft 2 in height 15.8 m 51 ft 10 in
44.84 m 147 ft 1 in wingspan 43.9 m 144 ft
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan
56,000lb to 61,500lb thrust per engine 52,000 lb
112,000–123,000 lb total thrust 104,000 lb
171,700 kg 378,600 lb MTOW 148,768 kg 328,000 lb
7,500 km 4,052 nm range 8,050 km 4,348 nm
897 km/h 557 mph cruise speed 482 knots 279 mph
210-250 passengers capacity 190-230 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.