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Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For
- Aerospace Standard
Published January 03, 2011 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification covers the design and installation requirements for Types I and II military aircraft hydraulic systems.
AS5440 has been updated to Revision A for the following reasons:
Minor technical changes have been made
The references called up in the document have been updated
Editorial changes have been made to improve the readability of the document
|Aerospace Standard||Aerospace - Design and Installation of Commercial Transport Aircraft Hydraulic Systems|
|Aerospace Standard||Aerospace - Impulse Testing of Hydraulic Components|
|Aerospace Standard||Hydraulic System Components, Aircraft and Missiles, General Specification For|
Data Sets - Support Documents
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|Unnamed Dataset 5|
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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|
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.
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