Airbus A220-100 vs. Boeing CH-47 Chinook

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Airbus A220-100 versus Boeing CH-47 Chinook
35.0 m 114 ft 10 in length 15.88 m 51 feet 2 inches
11.5 m 37 ft 9 in height 5.68 m 18 feet 7.8 inches
35.1 m 115 ft 2 in wingspan
2 Turbofans (wing mounted) engines 2 x Honeywell T55-GA-714A turboshaft engines
21,000–23,000 lb thrust per engine 4,868 hp
42,000–46,000 lb total thrust 9,736 hp
63,100 kg 139,100 lb MTOW 22,680 kg 50,000 lb
6,390 km 3,451 nm range 370 km 200 nm
871 km/h 541 mph cruise speed 259 km/h 161 mph
Typical seating 2-class 100-120 capacity 33-55
rotor diameter 18.3 m 60 ft
rate of climb 10.2 m/s 2,008 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.