• 91/83289 DC : DRAFT DEC 1991

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

    PREN 3624 - AEROSPACE SERIES - POLYSULPHIDE SEALANTS, TWO-COMPONENT - TECHNICAL SPECIFICATION

    Available format(s): 

    Withdrawn date:  22-07-2013

    Language(s): 

    Published date:  23-11-2012

    Publisher:  British Standards Institution

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    Comment Closes On
    Committee ACE/65/-/25
    Document Type Draft
    Publisher British Standards Institution
    Status Withdrawn

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

    MIL L 7808 : K (1) LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
    MIL L 23699 : E LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE
    MIL-C-27725 Revision B:1969 COATING, CORROSION PREVENTIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS
    DIN EN 2133:2011-05 Aerospace series - Cadmium plating of steels with specified tensile strength
    EN 3456:2012 Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Sheet and strip, hot rolled — a ≤ 6 mm
    DIN EN 2120:1980-11 (Draft) AEROSPACE; STEEL FE-PA 12, SOFTENED AND COLD DRAWN, BARS AND WIRES 0,25 MM = D = 2,5 MM
    DIN EN 2212:1980-11 (Draft) Aerospace; steel FE-PL 43 S, 670 MPa
    EN 2437 : 2001 AEROSPACE SERIES - CHROMATE CONVERSION COATINGS (YELLOW) FOR ALUMINIUM AND ALUMINIUM ALLOYS
    DIN EN 3042:1992-02 AEROSPACE SERIES - QUALITY ASSURANCE, EN AEROSPACE PRODUCTS - QUALIFICATION PROCEDURE
    EN 2338 : 2001 Aerospace series - Sheets, hot rolled in titanium and titanium alloys - Thickness 0,8 mm < = a < = 6 mm - Dimensions
    ISO 2768-2:1989 GENERAL TOLERANCES - PART 2: GEOMETRICAL TOLERANCES FOR FEATURES WITHOUT INDIVIDUAL TOLERANCE INDICATIONS
    EN 2101 : 1991 AEROSPACE SERIES - CHROMIC ACID ANODIZING OF ALUMINIUM AND WROUGHT ALUMINIUM ALLOYS
    EN 3102:2013 Aerospace series - Sealants - Test methods - Determination of low-temperature flexibility
    EN 4120:2004 Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated on thread - Classification: 1 210 MPa (at ambient temperature) / 730 °C
    EN 2589 : 2017 AEROSPACE SERIES - STEEL - SHEET AND STRIP, COLD ROLLED - THICKNESS 0,1 MM <= A <= 3 MM - DIMENSIONS
    MIL H 5606 : G HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE
    ISO 554:1976 Standard atmospheres for conditioning and/or testing — Specifications
    EN 2090 : 2005 AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024 - T3 - CLAD SHEET AND STRIP 0,3 MM <= A <= 6 MM
    EN 2590 : 2017 AEROSPACE SERIES - STEEL - SHEETS AND PLATES, HOT ROLLED - DIMENSIONS
    ISO 868:2003 Plastics and ebonite — Determination of indentation hardness by means of a durometer (Shore hardness)
    ISO 1817:2015 Rubber, vulcanized or thermoplastic Determination of the effect of liquids
    EN 3094:2017 Aerospace series - Sealants - Test method - Determination of the application time
    ISO 2781:2008 Rubber, vulcanized or thermoplastic Determination of density
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