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SAE International - AS5440A

Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For

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Organization: SAE International
Publication Date: 3 January 2011
Status: active
description:

This specification covers the design and installation requirements for Types I and II military aircraft hydraulic systems.

Document History

AS5440A
January 3, 2011
Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For
This specification covers the design and installation requirements for Types I and II military aircraft hydraulic systems.

References

This document references:
AIR4057 - SECONDARY FILTERS FOR FLUID SYSTEM RELIABILITY
Published by SAE International on May 1, 1994
It discusses the design choices and engineering trade-offs available to the system designer in the efficient selection and application of Last-Chance filters in contrast to main or primary system...
This document references:
AIR5829 - Air in Aircraft Hydraulic Systems
Published by SAE International on January 19, 2018
This SAE Aerospace Information Report (AIR) discusses the forms that air may take in aircraft hydraulic systems. Further, the effects of the various air forms on system operation are addressed....
This document references:
AMS3216 - FLUOROCARBON RUBBER Fuel and Oil Resistant 70 - 80
Published by SAE International on April 15, 1978
This specification covers a fluorocarbon rubber in the form of sheet, strip, tubing, molded shapes, and extrusions.
This document references:
AMS3218 - FLUOROCARBON (FKM) RUBBER High-Temperature-Fluid Resistant Low Compression Set 85 to 95
Published by SAE International on October 1, 1997
This specification covers a fluorocarbon (FKM) rubber in the form of sheet, strip, tubing, extrusions and molded shapes.
This document references:
AMS4081 - ALUMINUM ALLOY TUBING, HYDRAULIC 1.0Mg - 0.6Si - 0.25Cu - 0.25Cr (61S-T4)
Published by SAE International on June 1, 1952
A description is not available for this item.
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