Airbus A310-300 vs. Airbus A330-200
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Airbus A310-300 |
versus |
Airbus A330-200 |
46.66 m |
153 ft 1 in |
length |
58.82 m |
193 ft 0 in |
15.8 m |
51 ft 10 in |
height |
17.39 m |
57 ft 1 in |
43.9 m |
144 ft |
wingspan |
64 m |
210 ft |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
2 Turbofans |
52,000 lb |
thrust per engine |
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf |
104,000 lb |
total thrust |
Depends on the engine variant |
148,768 kg |
328,000 lb |
MTOW |
251,000 kg |
553,400 lb |
8,050 km |
4,348 nm |
range |
15,094 km |
8,150 nm |
482 knots |
279 mph |
cruise speed |
531 mph |
855 km/h |
190-230 passengers |
capacity |
220-260 |
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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.