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About This Item

 

Full Description

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).
 

Document History

  1. SAE ARP4835A

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    Recommended Design and Test Requirements for Hydraulic Thermal Expansion Relief Valves

    • Most Recent
  2. SAE ARP4835


    Aerospace Fluid Power-Hydraulic Thermal Expansion Relief Valves

    • Historical Version