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  • PREN 2491 : 200P1

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

    AEROSPACE SERIES - MOLYBDENUM DISULPHIDE DRY LUBRICANTS - COATING METHODS

    Available format(s):  Hardcopy, PDF

    Withdrawn date:  23-07-2013

    Language(s):  English

    Published date: 

    Publisher:  Aerospace & Defence Industries Association of Europe

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

    Foreword
    1 Scope
    2 Purpose of process
    3 Normative references
    4 Terms and definitions
    5 Apparatus
    6 Information for the processor
    7 Surface roughness of parts prior to application
    8 Surface preparation
    9 Coating
    10 Post-treatment
    11 Removal of the film
    12 Characteristics, requirements and test methods
    13 Quality assurance
    14 Acceptance
    15 Re-Treatment

    Abstract - (Show below) - (Hide below)

    Specifies the coating methods and characteristics of molybdenum disulphide dry film lubricants which may be applied to parts in titanium, titanium alloys, steel, corrosion resistant steel and nickel based alloys.

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

    Comment Closes On
    Document Type Draft
    Publisher Aerospace & Defence Industries Association of Europe
    Status Withdrawn

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

    PREN 2264 : 1995 AEROSPACE SERIES - NUTS, ANCHOR, SELF-LOCKING, FLOATING, TWO LUG, INCREMENTAL COUNTERBORE, IN ALLOY STEEL, CADMIUM PLATED, MOS2 LUBRICATED - CLASSIFICATION: 900 MPA (AT AMBIENT TEMPERATURE) / 235 DEGREES C
    PREN 3538 : 200P1 AEROSPACE SERIES - NUTS, ANCHOR, SELF-LOCKING, FIXED, TWO LUG, REDUCED SERIES, WITH COUNTERBORE, IN HEAT RESISTING STEEL, MOS[2] LUBRICATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/315 DEGREE C
    PREN 3566 : 200P1 AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30 MINUTES IN TITANIUM ALLOY - ADAPTERS WITH LOCKING RING
    DIN EN 3740:1996-11 AEROSPACE SERIES - BOLTS, SHOULDERED, THIN HEXAGONAL HEAD, CLOSE TOLERANCE SHANK, SHORT THREAD, IN TITANIUM ALLOY, ANODIZED, MOS[2] LUBRICATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/315 DEGREES C
    EN 2884:1996 Aerospace series - Screws, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C
    EN 3723 : 1996 AEROSPACE SERIES - NUTS, HEXAGONAL, SELF-LOCKING, IN HEAT RESISTING STEEL FE-PA92HT (A286), MOS[2] COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/425 DEGREE C
    EN 2870:1996/AC:1996 AEROSPACE SERIES - BOLTS, NORMAL BIHEXAGONAL HEAD, CLOSE TOLERANCE NORMAL SHANK, SHORT THREAD, IN TITANIUM ALLOY, ANODIZED, MOS[2] LUBRICATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/315 DEGREES C

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

    EN 9100:2009 Quality Management Systems - Requirements for Aviation, Space and Defense Organizations
    EN 2516:1997 Aerospace series - Passivation of corrosion resisting steels and decontamination of nickel base alloys
    TR 4070 : 1 AEROSPACE SERIES - MOLYBDENUM DISULPHIDE COATINGS - LIST OF COMMERCIAL PRODUCTS
    ISO 1463:2003 Metallic and oxide coatings Measurement of coating thickness Microscopical method
    EN 2133:2010 Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
    ISO 8080:1985 Aerospace Anodic treatment of titanium and titanium alloys Sulfuric acid process
    ISO 2431:2011 Paints and varnishes Determination of flow time by use of flow cups
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