Airbus A321-200 vs. Boeing CH-47 Chinook

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Airbus A321-200 versus Boeing CH-47 Chinook
44.51 m 146 ft 0 in length 15.88 m 51 feet 2 inches
11.76 m 38 ft 7 in height 5.68 m 18 feet 7.8 inches
35.8 m 117 ft 5 in wingspan
2 GE CFM56-5B3 engines 2 x Honeywell T55-GA-714A turboshaft engines
31,600 lbs thrust per engine 4,868 hp
63,200 lbs total thrust 9,736 hp
89,000 kg 196,200 lb MTOW 22,680 kg 50,000 lb
4,000 nmi 7,408 km range 370 km 200 nm
871 km/h 541 mph cruise speed 259 km/h 161 mph
185 to 220 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.