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.