• I.S. 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 DEGREES C - TECHNICAL SPECIFICATION

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  01-01-2008

    Publisher:  National Standards Authority of Ireland

    For Harmonized Standards, check the EU site to confirm that the Standard is cited in the Official Journal.
    Only cited Standards give presumption of conformance to New Approach Directives/Regulations.

    Dates of withdrawal of national standards are available from NSAI.

    Add To Cart

    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).

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

    Document Type Standard
    Publisher National Standards Authority of Ireland
    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
    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
    • Access your standards online with a subscription

      Features

      • Simple online access to standards, technical information and regulations
      • Critical updates of standards and customisable alerts and notifications
      • Multi - user online standards collection: secure, flexibile and cost effective