Airbus A321LR vs. Boeing CH-47 Chinook

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Airbus A321LR 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
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 2 x Honeywell T55-GA-714A turboshaft engines
Over 33,000 lbs (147 kN) thrust per engine 4,868 hp
66,000 lbs (294 kN) total thrust 9,736 hp
97,000 kg 213,800 lb MTOW 22,680 kg 50,000 lb
7,400 km 4,000 nm range 370 km 200 nm
832 km/h 517 mph cruise speed 259 km/h 161 mph
180-220 passengers 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.