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  • BS EN 3916:2008

    Current The latest, up-to-date edition.

    Aerospace series. Insert, thin wall. Salvage procedure for components

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  30-09-2008

    Publisher:  British Standards Institution

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    Table of Contents - (Show below) - (Hide below)

    Foreword
    1 Scope
    2 Normative references
    3 Conditions of use
    4 Re-machining of an existing insert hole
    5 Insert and tapped hole particulars
    6 Installation of oversize inserts
    7 Minimum criteria for the installation and removal
       tools and their methods of application
    8 Assembly drive tool and swage tool
    9 Assembly procedure
       9.1 Insertion
       9.2 Swaging
       9.3 Gauging and inspection
    10 Oversize insert removal, replacement and tools

    Abstract - (Show below) - (Hide below)

    Provides the accepted methods for the reclamation of installation holes for standard thin wall inserts, within assemblies.

    Scope - (Show below) - (Hide below)

    1.1 This specification covers the accepted methods for the reclamation of installation holes for standard thin wall inserts, within assemblies. 1.2 To enable rectification when defects or damage occur to the standard insert tapped installation hole, or to rectify any out of position of the hole within the specified parameters of use. 1.3 To control the machining of the existing insert hole and the installation requirements of the replacement oversize thin wall insert.

    General Product Information - (Show below) - (Hide below)

    Committee ACE/12
    Document Type Standard
    Publisher British Standards Institution
    Status Current

    Standards Referencing This Book - (Show below) - (Hide below)

    ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
    EN 3913:2007 Aerospace series - Insert, thin wall, self-locking, short, in heat resisting nickel base alloy NI-PH2601 (Ni-P100HT, Inconel 718), silver plated on internal thread, for salvage of components
    EN 3915 : 2008 Aerospace series - Insert, thin wall, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), for salvage of components - Classification: 1 275 MPa (at ambient temperature) / 550 °C - Technical specification
    EN 3676:1998 Aerospace series - Inserts, thin wall, self-locking - Design standard
    ISO 965-1:2013 ISO general purpose metric screw threads — Tolerances — Part 1: Principles and basic data
    EN 3914:2008 Aerospace series - Insert, thin wall, self-locking, long, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), silver plated on internal thread, for salvage of components
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