Airbus A220-100 vs. Boeing 747-8I
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Airbus A220-100 |
versus |
Boeing 747-8I |
35.0 m |
114 ft 10 in |
length |
76.25 m |
250 ft 2 in |
11.5 m |
37 ft 9 in |
height |
19.35 m |
63 ft 6 in |
35.1 m |
115 ft 2 in |
wingspan |
68.45 m |
224 ft 7 in |
2 Turbofans (wing mounted) |
engines |
4x General Electric GEnx 2B67 Turbofan |
21,000–23,000 lb |
thrust per engine |
66,500 pounds |
42,000–46,000 lb |
total thrust |
266,000 pounds |
63,100 kg |
139,100 lb |
MTOW |
443,613 kg |
977,500 lb |
6,390 km |
3,451 nm |
range |
8,000 nm |
14,816 km |
871 km/h |
541 mph |
cruise speed |
Mach 0.86 |
1,062 km/h |
Typical seating 2-class 100-120 |
capacity |
467 passengers (three-class configuration) |
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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.