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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.