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  • BS EN 2680:2006

    Current The latest, up-to-date edition.

    Aerospace series. Nuts, anchor, self-locking, floating, self-aligning, two lug, in alloy steel, cadmium plated, MoS2 lubricated. Classification: 900 MPa (at ambient temperature) / 235°C

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  30-06-2006

    Publisher:  British Standards Institution

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

    Foreword
    1 Scope
    2 Normative references
    3 Required characteristics
    4 Designation
    5 Marking
    6 Technical specification

    Abstract - (Show below) - (Hide below)

    Specifies the characteristics of self-locking, floating, self-aligning, two lug anchor nuts, in alloy steel, cadmium plated, MoS[2]-lubricated, metric series.

    Scope - (Show below) - (Hide below)

    This standard specifies the characteristics of self-locking, floating, self-aligning, two lug anchor nuts, in alloy steel, cadmium plated, MoS2-lubricated. Classification: 900 MPa / 235 °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)

    EN 9100:2009 Quality Management Systems - Requirements for Aviation, Space and Defense Organizations
    ISO 8788:2000 Aerospace Nuts, metric Tolerances of form and position
    ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
    EN 2491:2011 Aerospace series - Molybdenum disulphide dry lubricants - Coating methods
    ISO 12273:2010 Aerospace Nuts, anchor, self-locking, floating, self-aligning, two lug, with MJ threads, classifications: 900 MPa (at ambient temperature)/235 degrees C, 900 MPa (at ambient temperature)/315 degrees C and 900 MPa (at ambient temperature)/425 degrees C Dimensions
    ISO 5858:1999 Aerospace Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C Procurement specification
    EN 2133:2010 Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
    EN 2424:2008 Aerospace series - Marking of aerospace products
    ISO 9001:2015 Quality management systems — Requirements
    TR 3791 : 3 AEROSPACE SERIES - MATERIALS FOR SELF-LOCKING NUTS, THREADED INSERTS AND SCREW THREAD INSERTS OF TEMPERATURE CLASSES <= 425 DEGREES C
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