• BS EN 4826:2014

    Current The latest, up-to-date edition.

    Aerospace series. Zinc-Nickel (12 %-16 % Ni) plating of steels with specified tensile strength ≤ 1 450 MPa, copper alloys, nickel alloys and aluminium alloys for parts and fasteners

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  31-12-2014

    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 Purpose of process
    5 Applicability and limitations of the process
    6 Coating system classification
    7 Requirements
    8 Quality requirements
    9 Designation

    Abstract - (Show below) - (Hide below)

    Defines the plating of a Zinc-Nickel (12% to 16%) alloy on mechanical parts and fasteners in steels (R[m] <= 1450 MPa), stainless steels (R[m] <= 1450 MPa), copper alloys, nickel alloys and aluminium alloys (not applicable for electrical components), as well as the passivation and lubricant finishing that can be associated to them.

    Scope - (Show below) - (Hide below)

    This European Standard specifies the plating of a Zinc-Nickel (12%to 16%) alloy on mechanical parts and fasteners in steels ( R m≤1450MPa), stainless steels ( R m≤1450MPa), copper alloys, nickel alloys and aluminium alloys (not applicable for electrical components), as well as the passivation and lubricant finishing that can be associated to them. The Zinc-Nickel process is an electrolytic plating process under controlled current allowing to deposit a Zinc-Nickel layer from, most often, an alkaline electrolyte. Alkaline Zinc-Nickel is only considered in this standard.

    The purpose of this standard is to give technical and quality requirements of Zinc-Nickel plating. It doesn’t give complete in-house process instructions, these shall be given in the manufacturers detailed process instructions.

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

    Committee ACE/65
    Development Note Supersedes 12/30263299 DC. (01/2015)
    Document Type Standard
    Publisher British Standards Institution
    Status Current
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    15/30281806 DC : 0 BS A 401 TO A 420 - AEROSPACE SERIES - SPECIFICATION FOR SCREWS, PAN AND 100 DEGREES COUNTERSUNK HEAD, HEXALOBULAR DRIVE RECESS (UNIFIED THREADS BELOW 1/4 INCH), VARIOUS MATERIALS
    BS A 401-420:2015 Specification for screws, pan and 100° countersunk head, hexalobular drive recess (unified threads below ¼ inch) in various materials

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

    EN 9100:2009 Quality Management Systems - Requirements for Aviation, Space and Defense Organizations
    EN 4473:2010 Aerospace series - Aluminium pigmented coatings for fasteners - Technical specification
    EN 2832:1993 Aerospace series - Hydrogen embrittlement of steels - Notched specimen test
    EN ISO 3497 : 2000 METALLIC COATINGS - MEASUREMENTS OF COATING THICKNESS - X-RAY SPECTROMETRIC METHODS
    EN ISO 2409:2013 Paints and varnishes - Cross-cut test (ISO 2409:2013)
    ISO 1463:2003 Metallic and oxide coatings Measurement of coating thickness Microscopical method
    EN ISO 9227:2017 Corrosion tests in artificial atmospheres - Salt spray tests (ISO 9227:2017)
    NASM1312-14:1997 FASTENER TEST METHODS METHOD 14 STRESS DURABILITY, INTERNALLY THREADED
    ISO 2819:1980 Metallic coatings on metallic substrates — Electrodeposited and chemically deposited coatings — Review of methods available for testing adhesion
    ISO 3497:2000 Metallic coatings Measurement of coating thickness X-ray spectrometric methods
    ISO 9227:2017 Corrosion tests in artificial atmospheres — Salt spray tests
    ISO 2409:2013 Paints and varnishes Cross-cut test
    NASM1312-5:2012 FASTENER TEST METHODS METHOD 5 STRESS DURABILITY
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