Airbus A310-300 vs. Douglas DC-8-61

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Airbus A310-300 versus Douglas DC-8-61
46.66 m 153 ft 1 in length 57.0 m 187 ft 0 in
15.8 m 51 ft 10 in height 13.1 m 43 ft
43.9 m 144 ft wingspan 45.24 m 148 ft 5 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 4x P&W JT3D-3B Turbofan
52,000 lb thrust per engine 18,000 pound-force
104,000 lb total thrust 72,000 pound-force
148,768 kg 328,000 lb MTOW 147,400 kg 325,000 lb
8,050 km 4,348 nm range 3,200 nm 5,926 km
482 knots 279 mph cruise speed 483 knots 282 mph
190-230 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.