• BS EN 3899:2004

    Current The latest, up-to-date edition.

    Aerospace series. Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH). Technical specification

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  16-12-2004

    Publisher:  British Standards Institution

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

    Foreword
    1 Scope
    2 Normative references
    3 Terms and definitions
    4 Quality assurance
      4.1 Qualification
      4.2 Acceptance
          4.2.1 Purpose
          4.2.2 Conditions
          4.2.3 Responsibility
          4.2.4 Inspection and test report
    5 Requirements
    Annex A (normative) Definition of test block
    Annex B (normative) Assembly for rotational resistance test
    Annex C (normative) Axial tensile strength test
    Annex D (normative) Assembly for reusability test

    Abstract - (Show below) - (Hide below)

    Describes the characteristics, qualification and acceptance requirements for self-locking thickwall inserts with MJ threads, in FE-PM3801, for aerospace applications.

    Scope - (Show below) - (Hide below)

    This standard specifies the characteristics, qualification and acceptance requirements for self-locking thickwall inserts with MJ threads, in FE-PM3801, for aerospace applications. It is applicable whenever referenced.

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

    Committee ACE/12
    Development Note Supersedes 92/71354 DC (02/2003)
    Document Type Standard
    Publisher British Standards Institution
    Status Current
    Supersedes

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

    ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
    EN 4015:2004 Aerospace series - Inserts, thickwall, self-locking - Installation and removal procedure
    EN 4014:2004 Aerospace series - Inserts, thickwall, self-locking - Design standard
    ISO 3452:1984 Non-destructive testing — Penetrant inspection — General principles
    ISO 7481:2000 Aerospace — Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C — Test methods
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