Airbus A300-600 vs. Lockheed L-1011 TriStar 500

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Airbus A300-600 versus Lockheed L-1011 TriStar 500
54.10 m 177 ft 6 in length 50.05 m 164 ft 3 in
16.5 m 54 ft 2 in height 16.87 m 55 ft 4 in
44.84 m 147 ft 1 in wingspan 50.09 m 164 ft 4 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 3 Rolls-Royce RB211 engines
56,000lb to 61,500lb thrust per engine 42,000 lbf
112,000–123,000 lb total thrust 126,000 lbf (3 engines x 42,000 lbf per engine)
171,700 kg 378,600 lb MTOW 231,330 kg 510,000 lb
7,500 km 4,052 nm range 11,260 km 6,100 nm
897 km/h 557 mph cruise speed 525 knots 972 km/h
210-250 passengers capacity Max. 315 passengers (typical 253)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.