Airbus A310-300 vs. Lockheed L-1011 TriStar 500

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Airbus A310-300 versus Lockheed L-1011 TriStar 500
46.66 m 153 ft 1 in length 50.05 m 164 ft 3 in
15.8 m 51 ft 10 in height 16.87 m 55 ft 4 in
43.9 m 144 ft wingspan 50.09 m 164 ft 4 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 3 Rolls-Royce RB211 engines
52,000 lb thrust per engine 42,000 lbf
104,000 lb total thrust 126,000 lbf (3 engines x 42,000 lbf per engine)
148,768 kg 328,000 lb MTOW 231,330 kg 510,000 lb
8,050 km 4,348 nm range 11,260 km 6,100 nm
482 knots 279 mph cruise speed 525 knots 972 km/h
190-230 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.