This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent or other systems. This assembled coupling, hereafter referred to as the assembly, and is designed for use from −65 to +400 °F and at 125 psig nominal operating pressure. AS1650 Revision D returns vibration test to revision A test requirements. This revision encompasses changes to test specimen configurations, fixtures, fluid and vibration levels. Additionally, various changes were made to clarify proof and pressure surge test requirements.


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    Title :

    Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification


    Publication date :

    2017-07-10



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English