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 |
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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.