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This aerospace standard covers hose assemblies intended for use in aircraft high temperature fluid systems. The specified temperature range is -55~C (-67~F) to +204~C (400~F). Operating pressures are listed in Table 1. The assemblies shall be of the following types: Type I – non-conductive inner tube; and Type II – conductive inner tube. The hose assemblies shall be of the following classes: Class 1 – liquid proof test; and Class 2 – pneumatic proof test.

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Published:

08/21/2015

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1 file , 880 KB