Airbus A330-200 vs. McDonnell-Douglas DC-9-30
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Airbus A330-200 |
versus |
McDonnell-Douglas DC-9-30 |
58.82 m |
193 ft 0 in |
length |
36.36 m |
119 ft 3 in |
17.39 m |
57 ft 1 in |
height |
8.5 m |
27 ft 11 in |
64 m |
210 ft |
wingspan |
28.44 m |
93 ft 4 in |
2 Turbofans |
engines |
2x Pratt & Whitney JT8D |
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 |
15,000 pound-force |
Depends on the engine variant |
total thrust |
30,000 pound-force (2 engines) |
251,000 kg |
553,400 lb |
MTOW |
54,885 kg |
121,000 lb |
15,094 km |
8,150 nm |
range |
2,632 km |
1,422 nm |
531 mph |
855 km/h |
cruise speed |
898 km/h |
558 mph |
220-260 |
capacity |
Up to 139 passengers |
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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.