Airbus A321XLR vs. Douglas DC-8

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Airbus A321XLR versus Douglas DC-8
44.51 m 146 ft 0 in length 57.10 m 187 ft 4 in
11.76 m 38 ft 7 in height 16.84 m 55 ft 3 in
35.8 m 117 ft 5 in wingspan 45.24 m 148 ft 5 in
CFM LEAP-1A and P&W PW1100G engines 4 x Pratt & Whitney JT3D turbofan engines
33,000 lbs (147 kN) thrust per engine Approximately 17,000 lbf per engine
66,000 lbs (294 kN) total thrust Approximately 68,000 lbf total
101,000 kg 222,700 lb MTOW 158,760 kg 350,000 lb
4,700 nmi 8,704 km range 11,918 km 6,437 nm
963km/h 598mph cruise speed 900 km/h 559 mph
180-220 seats (typical 2-class seating) capacity Up to 259 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.