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  • BS EN 3915:2008

    Current The latest, up-to-date edition.

    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: 1275 MPa (at ambient temperature) / 550°C. Technical specification

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  30-05-2008

    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
          4.1.1 Purpose
          4.1.2 EN 9133
      4.2 Acceptance
          4.2.1 Purpose
          4.2.2 Conditions
          4.2.3 Responsibility
          4.2.4 Inspection and test report
    5 Requirements

    Abstract - (Show below) - (Hide below)

    Describes the characteristics, qualification and acceptance requirements for self-locking thin wall salvage inserts with MJ threads in NI-PH2601 (NI-P100HT).

    Scope - (Show below) - (Hide below)

    This standard specifies the characteristics, qualification and acceptance requirements for self-locking thin wall salvage inserts with MJ threads in NI-PH2601 (NI P100HT). Classification: 1 275 MPa ) / 550 °C ).

    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 3534:1977 Statistics — Vocabulary and symbols
    ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
    EN ISO 4288 : 1997 GEOMETRICAL PRODUCT SPECIFICATIONS (GPS) - SURFACE TEXTURE: PROFILE METHOD - RULES AND PROCEDURES FOR THE ASSESSMENT OF SURFACE TEXTURE
    PREN 4376 : 200P1 AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 200 MM
    ISO 3452:1984 Non-destructive testing — Penetrant inspection — General principles
    EN 3298:2008 Aerospace series - Inserts, thin wall, self-locking - Installation and removal procedure
    EN 3676:1998 Aerospace series - Inserts, thin wall, self-locking - Design standard
    PREN 4377 : 200P1 AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) - NON HEAT TREATED - FORGING STOCK - A OR D <= 300 MM
    PREN 2404 : 2 AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NI-P100-HT - SOLUTION TREATED AND PRECIPITATION TREATED - BARS
    SAE AMS 4117 : 2015 ALUMINUM ALLOY, ROLLED OR COLD FINISHED BARS, RODS, AND WIRE AND FLASH WELDED RINGS, 1.0MG - 0.60SI - 0.28CU - 0.20CR (6061; -T6, -T651)
    SAE AMS QQ A 225/8 : 1998 ALUMINUM ALLOY 6061, BAR, ROD, WIRE, AND SPECIAL SHAPES; ROLLED, DRAWN, OR COLD FINISHED
    ISO 8642:2008 Aerospace — Self-locking nuts with maximum operating temperature greater than 425 degrees C — Test methods
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