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