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Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For
- Aerospace Standard
- AS5440A
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers the design and installation requirements for Types I and II military aircraft hydraulic systems.
Rationale
AS5440 has been updated to Revision A for the following reasons:
-
a
Minor technical changes have been made
-
b
The references called up in the document have been updated
-
c
Editorial changes have been made to improve the readability of the document
Recommended Content
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Topic
Data Sets - Support Documents
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TABLE 1 | SYSTEM PEAK PRESSURE | |
TABLE 2 | HYDRAULIC PRESSURE | |
TABLE 3 | HYDRAULIC LINE SUPPORT SPACING, U.S. CUSTOMARY | |
TABLE 4 | HYDRAULIC LINE SUPPORT SPACING, METRIC | |
TABLE 5 | DATA REQUIREMENTS |
Issuing Committee
A-6A2 Military Aircraft Committee
The Military Aircraft Panel is responsible for the development of standards and recommended practices related to the integration of fluid power and actuation technologies into military air vehicles. The panel provides a forum for government engineers, prime contractors, suppliers, and fleet support representatives to exchange technical information and discuss regulatory updates, recent technology developments, lessons learned, and issues related to system development and in service operation.
Reference
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