I read the engine seperated from its pylon, and flipped over the wing, severing the Hydraluic lines, and when the pilot selected retract, the slats and flaps could not, and gradually moved all the way "Down/out" causing aysmmetric thrust and the crash. Have newer aircraft fixed that design, or does a loss of pressure cause the Flaps and Slats to extend, needed or not? It was a DC-10-10,1979 was the year. What are the usual check offs for a such a catastrophic loss (physical that is, the engine has departed the wing) in such a situation?
2007-10-08
13:43:01
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10 answers
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asked by
gregva2001
3