This aerospace specification 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, is designed for use from -65 to +400 °F and at 125 psig nominal operating pressure. AS1650 Rev. B corrects the placement and title of paragraph 4.6.6. Revision B adds PRI QPL/QML requirements, deletes gunfire vibration requirements, reduces impulse peak pressure requirements and provides a general document update.


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    Title :

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


    Publication date :

    2010-08-24



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English