Airbus A310-300 vs. Douglas DC-7

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Airbus A310-300 versus Douglas DC-7
46.66 m 153 ft 1 in length 34.00 m 111 ft 6 in
15.8 m 51 ft 10 in height 8.38 m 27 ft 6 in
43.9 m 144 ft wingspan 35.8 m 117 ft 5 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 4 x Wright R-3350 Duplex-Cyclone radial engines
52,000 lb thrust per engine Approximately 3,400 hp per engine
104,000 lb total thrust Approximately 13,600 hp total
148,768 kg 328,000 lb MTOW 90,718 kg 200,000 lb
8,050 km 4,348 nm range 6,250 km 3,375 nm
482 knots 279 mph cruise speed 507 km/h 315 mph
190-230 passengers capacity Up to 105 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.