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Thread: SWA1380 - diversion to KPHL after engine event
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Old 29th Apr 2018, 01:38
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CONSO
 
Join Date: Mar 2014
Location: WA STATE
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Cool
Originally Posted by lomapaseo
One of the impediments against the early SST proposals was the cruise altitude vs decompression rate vs the size of the holes made by a bursting turbine disk.
perhaps this may help ?

https://www.faa.gov/documentLibrary/...r/AC_25-20.pdf
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