Airbus A320-200 vs. Lockheed L-1011 TriStar 500

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Airbus A320-200 versus Lockheed L-1011 TriStar 500
38.7 m 127 ft 0 in length 50.05 m 164 ft 3 in
17.4 m 57 ft 1 in height 16.87 m 55 ft 4 in
35.8 m 117 ft 5 in wingspan 50.09 m 164 ft 4 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 3 Rolls-Royce RB211 engines
Between 21,000 - 33,000 lbf thrust per engine 42,000 lbf
Between 42,000 - 66,000 lbf total thrust 126,000 lbf (3 engines x 42,000 lbf per engine)
77,000 kg 169,800 lb MTOW 231,330 kg 510,000 lb
5,700 km 3,078 nm range 11,260 km 6,100 nm
530 mph 853 km/h cruise speed 525 knots 972 km/h
Typically between 140-180 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.