This SAE Aerospace Standard (AS) establishes the requirements for port preparation, installation and removal procedure for AS5550 fitting assembly and AS5865 fitting reducer assembly, and is applicable when specified on engineering drawings, or in procurement documents.
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.
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.
This SAE Aerospace Standard (AS) establishes the requirements for port preparation, installation and removal procedure for AS5550 fitting assembly and AS5865 fitting reducer assembly, and is applicable when specified on engineering drawings, or in procurement documents.