Airbus A310-300 vs. Douglas DC-6

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Airbus A310-300 versus Douglas DC-6
46.66 m 153 ft 1 in length 32.18 m 105 ft 7 in
15.8 m 51 ft 10 in height 8.94 m 29 ft 4 in
43.9 m 144 ft wingspan 35.81 m 117 ft 6 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 4 x Pratt & Whitney R-2800-CB17 radial engines
52,000 lb thrust per engine Approximately 2,500 hp per engine
104,000 lb total thrust Approximately 10,000 hp total
148,768 kg 328,000 lb MTOW 52,200 kg 115,100 lb
8,050 km 4,348 nm range 5,800 km 3,133 nm
482 knots 279 mph cruise speed 507 km/h 315 mph
190-230 passengers capacity Up to 102 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.