This SAE Aerospace Standard (AS) establishes the requirements for 24??one AS5827 or EN 6123 flareless Ring locked fitting assemblies per AS5550 and AS5865@ for use in aircraft fluid systems at nominal operating pressure of 5080 psi maximum and operating temperature range of -65 to +275 ?? The general requirements shall be for@ but not limited to@ commercial aircraft hydraulic components per AS4941@ using port configuration as specified in AS5551. Classifications: Type 1 Standard requirement for Proof@ Tensile@ Fire@ and Vibration Test Type 2 Alternate requirement for Proof@ Tensile@ Fire@ and Vibration Test NOTE: Type 1 meets requirements of both types.
SAE AS5000-2006 history
2020SAE AS5000E-2020 Fitting, Plug-in Union, Ring Locked, 24 Degree Cone, Fluid Connection, 5080 psi (35000 kPa), Specification for
2013SAE AS5000D-2013 Fitting@ Plug-in Union@ Ring Locked@ 24 Degree Cone@ Fluid Connection@ 5080 psi (35 000 kPa)@ Specification for
2010SAE AS5000C-2010 Fitting@ Plug-in Union@ Ring Locked@ 24 Degree Cone@ Fluid Connection@ 5080 psi (35 000 kPa)@ Specification for
2008SAE AS5000B-2008 Fitting@ Plug-in Union@ Ring Locked@ 24° Cone@ Fluid Connection@ 5080 psi@ Specification for
2006SAE AS5000A-2006 Fitting, Plug-in Union, Ring Locked, 24° cone, Fluid Connection, 5080 psi, Specification for
2006SAE AS5000-2006 Fitting@ Plug-in Union@ Ring Locked@ 24° Cone@ Fluid Connection@ 5080 psi@ Specification for