SAE AS8775
Hydraulic System Components, Aircraft and Missiles, General Specification for
inactive
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| Organization: | SAE |
| Publication Date: | 1 July 1998 |
| Status: | inactive |
| Page Count: | 28 |
scope:
SCOPE:
Scope:
This specification covers the general requirements that are common to most hydraulic components (see 6.2), used in aeronautical hydraulic systems (see 6.1).
Classification:
Aircraft hydraulic systems in which components covered by this specification are to be used shall be of the following types, as specified:
Type I −65° to +160°F fluid temperature range
Type II −65° to +275°F fluid temperature range
Document History
July 1, 1998
Hydraulic System Components, Aircraft and Missiles, General Specification For
This specification covers the general requirements that are common to most hydraulic components (see 6.2), used in aeronautical hydraulic systems (see 6.1).
SAE AS8775
July 1, 1998
Hydraulic System Components, Aircraft and Missiles, General Specification for
SCOPE: Scope: This specification covers the general requirements that are common to most hydraulic components (see 6.2), used in aeronautical hydraulic systems (see 6.1). Classification: Aircraft...