Airbus A220-100 vs. Lockheed L-1011 TriStar 500

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Airbus A220-100 versus Lockheed L-1011 TriStar 500
35.0 m 114 ft 10 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 Turbofans (wing mounted) 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)
63,100 kg 139,100 lb MTOW 231,330 kg 510,000 lb
6,390 km 3,451 nm range 11,260 km 6,100 nm
871 km/h 541 mph cruise speed 525 knots 972 km/h
Typical seating 2-class 100-120 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.