SAE ARP4835-2006 PDF

Scope: This SAE Aerospace Recommended Practice (ARP) establishes the general requirements for hydraulic thermal expansion relief valves used in aircraft and missile hydraulic systems having operating pressures and temperatures as identified.

SAE ARP4835-2006 Referenced Document

SAE ARP1383B-2003 (R) Impulse Testing of Aerospace Hydraulic Actuators, Valves, Pressure Containers, and Similar Fluid System Components
SAE AS1241C-1997 (R) Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft
SAE AS1290A-1986 Graphic Symbols for Aircraft Hydraulic and Pneumatic Systems
SAE AS33514-1998 Fitting End@ Standard Dimensions for Flareless Tube Connection and Gasket Seal
SAE AS4059E-2005 (R) Aerospace Fluid Power - Cleanliness Classification for Hydraulic Fluids
SAE AS478M-2006 Identification Marking Methods
SAE AS4941-1998 Aerospace - General Requirements for Commercial Aircraft Hydraulic Components
SAE AS5202-2001 Port or Fitting End, Internal Straight Thread, Design Standard FSC 4730
SAE AS5440-1998 Hydraulic Systems, Aircraft, Design and Installation Requirements for FSC 1650; Should Be Used Instead of MIL-H-5440H, Which Was Cancelled on 13 September 1999
SAE AS8775-1998 Hydraulic System Components, Aircraft and Missiles, General Specification for Should Be Used Instead of MIL-H-8775D, which Was Cancelled on 28 September, 1998

2021 SAE ARP4835A-2021 Recommended Design and Test Requirements for Hydraulic Thermal Expansion Relief Valves
2006 SAE ARP4835-2006 Aerospace Fluid Power-Hydraulic Thermal Expansion Relief Valves