Airbus A320-200 vs. Douglas DC-8-61

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Airbus A320-200 versus Douglas DC-8-61
38.7 m 127 ft 0 in length 57.0 m 187 ft 0 in
17.4 m 57 ft 1 in height 13.1 m 43 ft
35.8 m 117 ft 5 in wingspan 45.24 m 148 ft 5 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 4x P&W JT3D-3B Turbofan
Between 21,000 - 33,000 lbf thrust per engine 18,000 pound-force
Between 42,000 - 66,000 lbf total thrust 72,000 pound-force
77,000 kg 169,800 lb MTOW 147,400 kg 325,000 lb
5,700 km 3,078 nm range 3,200 nm 5,926 km
530 mph 853 km/h cruise speed 483 knots 282 mph
Typically between 140-180 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.