Airbus A330-200 vs. Douglas DC-8-61
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Airbus A330-200 |
versus |
Douglas DC-8-61 |
58.82 m |
193 ft 0 in |
length |
57.0 m |
187 ft 0 in |
17.39 m |
57 ft 1 in |
height |
13.1 m |
43 ft |
64 m |
210 ft |
wingspan |
45.24 m |
148 ft 5 in |
2 Turbofans |
engines |
4x P&W JT3D-3B Turbofan |
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf |
thrust per engine |
18,000 pound-force |
Depends on the engine variant |
total thrust |
72,000 pound-force |
251,000 kg |
553,400 lb |
MTOW |
147,400 kg |
325,000 lb |
15,094 km |
8,150 nm |
range |
3,200 nm |
5,926 km |
531 mph |
855 km/h |
cruise speed |
483 knots |
282 mph |
220-260 |
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.