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  • NF EN 2862 : 2010

    Current The latest, up-to-date edition.

    AEROSPACE SERIES - NUTS, ANCHOR, SELF-LOCKING, FIXED, 90 DEGREES CORNER, WITH COUNTERBORE, IN ALLOY STEEL, CADMIUM PLATED, MOS[2] LUBRICATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/235 DEGREES C

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    Published date:  12-01-2013

    Publisher:  Association Francaise de Normalisation

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    Development Note Indice de classement: L24-480. PR NF EN 2862 July 2009. (07/2009)
    Document Type Standard
    Publisher Association Francaise de Normalisation
    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 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
    ISO 3221:1998 Aerospace Nuts, anchor, self-locking, fixed, 90 degrees corner, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C Dimensions
    EN 2424:2008 Aerospace series - Marking of aerospace products
    EN 2542:2008 Aerospace series - Steel FE-PL1502 (25CrMo4) - Annealed - Bar and wire - De ≤ 40 mm - For prevailing torque nuts
    EN 2543 : 2009 AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - ANNEALED - SHEET AND STRIP - 0,3 MM <= A <= 2 MM - FOR PREVAILING TORQUE NUTS
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