Airbus A321XLR vs. Boeing CH-47 Chinook

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Airbus A321XLR 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 LEAP-1A and P&W PW1100G engines 2 x Honeywell T55-GA-714A turboshaft engines
33,000 lbs (147 kN) thrust per engine 4,868 hp
66,000 lbs (294 kN) total thrust 9,736 hp
101,000 kg 222,700 lb MTOW 22,680 kg 50,000 lb
4,700 nmi 8,704 km range 370 km 200 nm
963km/h 598mph cruise speed 259 km/h 161 mph
180-220 seats (typical 2-class seating) 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.