Airbus A321XLR vs. Lockheed L-1011 TriStar 500

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Airbus A321XLR versus Lockheed L-1011 TriStar 500
44.51 m 146 ft 0 in length 50.05 m 164 ft 3 in
11.76 m 38 ft 7 in height 16.87 m 55 ft 4 in
35.8 m 117 ft 5 in wingspan 50.09 m 164 ft 4 in
CFM LEAP-1A and P&W PW1100G engines 3 Rolls-Royce RB211 engines
33,000 lbs (147 kN) thrust per engine 42,000 lbf
66,000 lbs (294 kN) total thrust 126,000 lbf (3 engines x 42,000 lbf per engine)
101,000 kg 222,700 lb MTOW 231,330 kg 510,000 lb
4,700 nmi 8,704 km range 11,260 km 6,100 nm
963km/h 598mph cruise speed 525 knots 972 km/h
180-220 seats (typical 2-class seating) 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.