Airbus A330-300 vs. Douglas DC-8-61
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Airbus A330-300 |
versus |
Douglas DC-8-61 |
63.66 m |
208 ft 9 in |
length |
57.0 m |
187 ft 0 in |
16.79 m |
55 ft 1 in |
height |
13.1 m |
43 ft |
60.3 m |
197 ft 9 in |
wingspan |
45.24 m |
148 ft 5 in |
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 |
engines |
4x P&W JT3D-3B Turbofan |
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) |
thrust per engine |
18,000 pound-force |
Depends on the engine type |
total thrust |
72,000 pound-force |
242,000 kg |
533,600 lb |
MTOW |
147,400 kg |
325,000 lb |
11,750 km |
6,346 nm |
range |
3,200 nm |
5,926 km |
900 km/h |
559 mph |
cruise speed |
483 knots |
282 mph |
250-290 |
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.