Airbus A321LR vs. Douglas DC-8-61

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Airbus A321LR 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 International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 4x P&W JT3D-3B Turbofan
Over 33,000 lbs (147 kN) thrust per engine 18,000 pound-force
66,000 lbs (294 kN) total thrust 72,000 pound-force
97,000 kg 213,800 lb MTOW 147,400 kg 325,000 lb
7,400 km 4,000 nm range 3,200 nm 5,926 km
832 km/h 517 mph cruise speed 483 knots 282 mph
180-220 passengers 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.