Airbus A220-300 vs. Lockheed L-1011 TriStar 500

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Airbus A220-300 versus Lockheed L-1011 TriStar 500
38.7 m 127 ft 0 in length 50.05 m 164 ft 3 in
11.5 m 37 ft 9 in height 16.87 m 55 ft 4 in
35.1 m 115 ft 2 in wingspan 50.09 m 164 ft 4 in
2 x Pratt & Whitney PurePower PW1500G engines 3 Rolls-Royce RB211 engines
21,000–23,000 lb thrust per engine 42,000 lbf
42,000–46,000 lb total thrust 126,000 lbf (3 engines x 42,000 lbf per engine)
70,900 kg 156,300 lb MTOW 231,330 kg 510,000 lb
6,297 km 3,402 nm range 11,260 km 6,100 nm
Mach 0.82 101,3 km/h cruise speed 525 knots 972 km/h
Typical seating 2-class 120-150 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.