Airbus A310-300 vs. Douglas C-54 Skymaster

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Airbus A310-300 versus Douglas C-54 Skymaster
46.66 m 153 ft 1 in length 28.60 m 93 ft 10 in
15.8 m 51 ft 10 in height 8.38 m 27 ft 6 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-2000 Twin Wasp radial engines
52,000 lb thrust per engine 1,200 to 1,450 horsepower (895 to 1,080 kW)
104,000 lb total thrust 4,800 to 5,800 horsepower
148,768 kg 328,000 lb MTOW 29,484 kg 65,000 lb
8,050 km 4,348 nm range 6,500 km 3,510 nm
482 knots 279 mph cruise speed 340 km/h 211 mph
190-230 passengers capacity Up to 50 passengers or 28,500 lb cargo
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.