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  • SAE AS 4751 : 2005

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    COUPLING ASSEMBLY, V-BAND SHEET METAL WIDE FLANGE, PNEUMATIC TUBE

    Available format(s):  Hardcopy, PDF

    Superseded date:  29-02-2024

    Language(s):  English

    Published date:  01-01-2005

    Publisher:  SAE International

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

    1 SCOPE
    2 APPLICABLE DOCUMENTS
    3 TECHNICAL REQUIREMENTS
    4 QUALITY ASSURANCE PROVISIONS
    5 PREPARATION FOR DELIVERY
    6 NOTES

    Abstract - (Show below) - (Hide below)

    This SAE Aerospace Standard (AS) establishes the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft pneumatic systems.

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

    Committee G-3
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By

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

    SAE AIR 869 : 2014 V-COUPLINGS, INCLUDING V-BAND AND V-RETAINER COUPLING ASSEMBLIES, FLANGE AND SEAL DESIGN, APPLICATION OF

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

    SAE AMS 5737 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS AND TUBING, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1650 DEGREES F (899 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED
    SAE AMS 5525 : 2012 STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, 1800 DEGREE F (982 DEGREE C) SOLUTION HEAT TREATED
    MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    SAE AIR 869 : 2014 V-COUPLINGS, INCLUDING V-BAND AND V-RETAINER COUPLING ASSEMBLIES, FLANGE AND SEAL DESIGN, APPLICATION OF
    MIL-HDBK-831 Revision A:2013 PREPARATION OF TEST REPORTS
    SAE AMS 5513 : 2015 STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 19CR - 9.2NI (SAE 30304), SOLUTION HEAT TREATED
    SAE AMS 5516 : 2012 STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 18CR - 9.0NI (SAE 30302), SOLUTION HEAT TREATED
    NASM25027:2012 NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F
    SAE AMS W 6858 : 2000 WELDING, RESISTANCE: SPOT AND SEAM
    SAE AMS 5510S : 2014 STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP AND PLATE, 18CR - 10.5NI - 0.40TI (SAE 30321) SOLUTION HEAT TREATED
    SAE AMS 5732 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED 1800 DEGREES F (982 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED
    AWS D17.1 : 2001 SPECIFICATION FOR FUSION WELDING FOR AEROSPACE APPLICATIONS
    SAE AS 8879 : 2004 SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER
    SAE AMS 5901B:2008 STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 18CR - 8NI (SAE 30301), SOLUTION HEAT TREATED
    SAE AMS 5518 : 2014 STEEL, CORROSION RESISTANT, SHEET AND STRIP 18CR - 8NI COLD ROLLED, 150 KSI (1034 MPA) TENSILE STRENGTH
    SAE AS 478 : 2015 IDENTIFICATION MARKING METHODS
    ASME Y14.100 : 2017 ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES
    NASM7873:2012 NUT, SELF-LOCKING, 1,200 DEGREES F
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