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Parts and Components Assembling G-3C, AS-EN Harmonization Task Group

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Standard

Fitting, Plug-in Union, Ring Locked, 24 Degree Cone, Fluid Connection, 5080 psi (35 000 kPa), Specification for
2013-08-12
HISTORICAL
AS5000D
This SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone 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 (35 000 kPa) maximum and operating temperature range of −65 to +275 °F (−54 to +135 °C). The general requirements shall be for, but not limited to, commercial aircraft hydraulic components per AS4941, using port configuration as specified in AS5551.
Standard

Fitting, Plug-in Union, Ring Locked, 24° Cone, Fluid Connection, 5080 psi, Specification for
2008-06-09
HISTORICAL
AS5000B
This SAE Aerospace Standard (AS) establishes the requirements for 24° cone 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 °F. The general requirements shall be for, but not limited to, commercial aircraft hydraulic components per AS4941, using port configuration as specified in AS5551.
Standard

Fitting, Plug-in Union, Ring Locked, 24° Cone, Fluid Connection, 5080 psi, Specification for
2006-03-22
HISTORICAL
AS5000
This SAE Aerospace Standard (AS) establishes the requirements for 24° cone 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 °F. The general requirements shall be for, but not limited to, commercial aircraft hydraulic components per AS4941, using port configuration as specified in AS5551.
Standard

Fitting, Plug-in Union, Ring Locked, 24° Cone, Fluid Connection, 5080 psi, Specification for
2006-11-14
HISTORICAL
AS5000A
This SAE Aerospace Standard (AS) establishes the requirements for 24° cone 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 °F. The general requirements shall be for, but not limited to, commercial aircraft hydraulic components per AS4941, using port configuration as specified in AS5551.
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