Airbus A321XLR vs. Douglas DC-8-61

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Airbus A321XLR versus Douglas DC-8-61
44.51 m 146 ft 0 in length 57.0 m 187 ft 0 in
11.76 m 38 ft 7 in height 13.1 m 43 ft
35.8 m 117 ft 5 in wingspan 45.24 m 148 ft 5 in
CFM LEAP-1A and P&W PW1100G engines 4x P&W JT3D-3B Turbofan
33,000 lbs (147 kN) thrust per engine 18,000 pound-force
66,000 lbs (294 kN) total thrust 72,000 pound-force
101,000 kg 222,700 lb MTOW 147,400 kg 325,000 lb
4,700 nmi 8,704 km range 3,200 nm 5,926 km
963km/h 598mph cruise speed 483 knots 282 mph
180-220 seats (typical 2-class seating) capacity 180 to 220 passengers in a mixed-class seating
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.