Airbus A300-600 vs. McDonnell-Douglas DC-9-30
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Airbus A300-600 |
versus |
McDonnell-Douglas DC-9-30 |
54.10 m |
177 ft 6 in |
length |
36.36 m |
119 ft 3 in |
16.5 m |
54 ft 2 in |
height |
8.5 m |
27 ft 11 in |
44.84 m |
147 ft 1 in |
wingspan |
28.44 m |
93 ft 4 in |
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 |
engines |
2x Pratt & Whitney JT8D |
56,000lb to 61,500lb |
thrust per engine |
15,000 pound-force |
112,000–123,000 lb |
total thrust |
30,000 pound-force (2 engines) |
171,700 kg |
378,600 lb |
MTOW |
54,885 kg |
121,000 lb |
7,500 km |
4,052 nm |
range |
2,632 km |
1,422 nm |
897 km/h |
557 mph |
cruise speed |
898 km/h |
558 mph |
210-250 passengers |
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.