Airbus A321XLR vs. McDonnell-Douglas DC-9-30

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Airbus A321XLR versus McDonnell-Douglas DC-9-30
44.51 m 146 ft 0 in length 36.36 m 119 ft 3 in
11.76 m 38 ft 7 in height 8.5 m 27 ft 11 in
35.8 m 117 ft 5 in wingspan 28.44 m 93 ft 4 in
CFM LEAP-1A and P&W PW1100G engines 2x Pratt & Whitney JT8D
33,000 lbs (147 kN) thrust per engine 15,000 pound-force
66,000 lbs (294 kN) total thrust 30,000 pound-force (2 engines)
101,000 kg 222,700 lb MTOW 54,885 kg 121,000 lb
4,700 nmi 8,704 km range 2,632 km 1,422 nm
963km/h 598mph cruise speed 898 km/h 558 mph
180-220 seats (typical 2-class seating) capacity Up to 139 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.