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) |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.