Name | Support | Language | Availability | Edition date | Price | ||
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PDF |
English |
Active |
8/26/2021 |
€116.00 |
|
Details
This Aerospace Recommended Practice (ARP) provides recommendations for the design and test requirements for a hydraulic thermal relief valve.
The thermal relief valve is intended for use in a civil or military aircraft hydraulic system with a rated system pressure up to 5000 psi (34500 kPa).
Additional Info
Author | Society of Automotive Engineers International (SAE) |
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Committee | A-6C5 Components Committee |
Published by | SAE |
Document type | Standard |
ICS | 49.080 : Aerospace fluid systems and components
|
Number of pages | 24 |
Replace | SAE ARP 4835:2006-09-13 |
Document history | SAE ARP 4835:2006-09-13 |
Keyword | SAE 4835,SAE ARP4835A,SAE ARP4835A,SAE ARP 4835 |