Airbus A300-600 vs. Piper PA-34 Seneca
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Airbus A300-600 |
versus |
Piper PA-34 Seneca |
54.10 m |
177 ft 6 in |
length |
8.71 m |
28 ft 7 in |
16.5 m |
54 ft 2 in |
height |
2.99 m |
9 ft 10 in |
44.84 m |
147 ft 1 in |
wingspan |
11.64 m |
38 ft 2 in |
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 |
engines |
2 x Continental IO-360 |
56,000lb to 61,500lb |
thrust per engine |
220 lbs |
112,000–123,000 lb |
total thrust |
440 lbs |
171,700 kg |
378,600 lb |
MTOW |
4,750 lb |
2,155 kg |
7,500 km |
4,052 nm |
range |
980 nm |
1,815 km |
897 km/h |
557 mph |
cruise speed |
165 kts |
103 mph |
210-250 passengers |
capacity |
5 |
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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.