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  • SAE AS 5127 : 2013

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    AEROSPACE STANDARD TEST METHODS FOR AEROSPACE SEALANTS METHODS FOR PREPARING AEROSPACE SEALANT TEST SPECIMENS

    Available format(s): 

    Superseded date:  17-11-2018

    Language(s): 

    Published date:  01-01-2013

    Publisher:  SAE International

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

    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. STANDARD TOLERANCES
    4. STANDARD CONDITIONS
    5. STANDARD HEAT CYCLES
    6. PREPARATION OF TEST SPECIMENS
    7. STANDARD TEST FLUIDS
    8. TEST METHODS
    9. NOTES

    Abstract - (Show below) - (Hide below)

    Describes the accepted methods used for preparing aerospace sealant test specimens for qualification and quality conformance or acceptance testing.

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

    Committee AMS G9
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

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

    SAE AS 5127/2 : 2014 TEST METHOD FOR AEROSPACE FIREWALL SEALANT FLAME PENETRATION
    SAE AMS 3281 : 2016 SEALING COMPOUND, POLYSULFIDE (T) SYNTHETIC RUBBER FOR INTEGRAL FUEL TANK AND FUEL CELL CAVITIES LOW DENSITY FOR INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C)
    SAE AMS 3265 : 2015 SEALING COMPOUND, POLYSULFIDE (T) RUBBER, FUEL RESISTANT, NON-CHROMATED CORROSION INHIBITING, FOR INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C)
    SAE AMS 3278 : 2016 SEALING AND COATING COMPOUND, POLYURETHANE (PUR), FUEL RESISTANT, HIGH TENSILE STRENGTH/ELONGATION, FOR INTEGRAL FUEL TANKS/FUEL CAVITIES/GENERAL PURPOSE
    SAE AMS 3379 : 2013(R2018) SEALING COMPOUND, POLYSULFIDE RUBBER PREFORMED STRIPS FOR SEALING REMOVABLE DOORS, SKINS, AND PANELS
    SAE AMS 3276 : 2016 SEALING COMPOUND, INTEGRAL FUEL TANKS AND GENERAL PURPOSE, INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C)
    SAE AMS 3102 : 2017 SEALING COMPOUND, POLYTHIOETHER RUBBER FAST CURING, LIGHT WEIGHT (SPECIFIC GRAVITY 0.78, MAX.) FOR INTEGRAL FUEL TANKS AND GENERAL PURPOSE, INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C)
    SAE AMS S 83318 : 2016 SEALING COMPOUND, POLYSULFIDE TYPE, LOW TEMPERATURE CURING, QUICK REPAIR, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES
    SAE AMS 3100 : 2013 ADHESION PROMOTER FOR POLYSULFIDE SEALING COMPOUNDS
    SAE AMS S 8802 : 2015 SEALING COMPOUND, FUEL RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES
    SAE AS 81550A : 2014 INSULATING COMPOUND, ELECTRICAL, EMBEDDING, REVERSION RESISTANT SILICONE
    SAE AMS 3376 : 2015 SEALING COMPOUND, NON-CURING, FLUOROSILICONE GROOVE INJECTION TEMPERATURE AND FUEL RESISTANT
    SAE AMS 3255 : 2017 SEALING TAPE, SHEET, OR GASKET, POLYTETRAFLUOROETHYLENE, EXPANDED (EPTFE) OIL AND WATER RESISTANT
    SAE AMS S 4383 : 2015 SEALING COMPOUND, TOPCOAT, FUEL TANK BUNA-N TYPE
    SAE AMS 3266 : 2017 SEALING COMPOUND, POLYTHIOETHER ELASTOMERIC TWO-PART ELECTRICALLY CONDUCTIVE
    SAE AMS 3381 : 2014 SEALING COMPOUND, AIRCRAFT FIREWALL, NON-SILICONE
    SAE AS 5127/1 : 2014 AEROSPACE STANDARD TEST METHODS FOR AEROSPACE SEALANTS TWO-COMPONENT SYNTHETIC RUBBER COMPOUNDS
    SAE AMS 3167 : 2005 SOLVENTS, WIPE FOR CLEANING PRIOR TO APPLICATION OF PRIMER AND TOP COAT MATERIALS, OR SEALING COMPOUNDS
    SAE AMS 3374 : 2013 SEALING COMPOUND AIRCRAFT FIREWALL, SILICONE
    SAE AMS 3277 : 2015 SEALING COMPOUND, POLYTHIOETHER RUBBER, FAST CURING FOR INTEGRAL FUEL TANKS AND GENERAL PURPOSE, INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C)
    SAE AMS 3284 : 2017 SEALING COMPOUND, LOW ADHESION, FOR REMOVABLE PANELS AND FUEL TANK INSPECTION PLATES

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

    SAE AMS C 27725 : 2016 COATING, CORROSION PREVENTATIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS, FOR USE TO 250 DEGREES F (121 DEGREES C)
    SAE AMS 4049 : 2016 ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD 5.6ZN - 2.5MG - 1.6CU - 0.23CR (ALCLAD 7075; -T6 SHEET - T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED
    SAE AMS 4911 : 2014 TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED
    SAE AS 5127/2 : 2014 TEST METHOD FOR AEROSPACE FIREWALL SEALANT FLAME PENETRATION
    SAE AMS3819C : 2007 CLOTHS, CLEANING, FOR AIRCRAFT PRIMARY AND SECONDARY STRUCTURAL SURFACES
    MIL-PRF-5425 Revision E:1998 PLASTIC SHEET, ACRYLIC, HEAT RESISTANT
    MIL-PRF-85285 Revision E:2012 COATING: POLYURETHANE, AIRCRAFT AND SUPPORT EQUIPMENT
    SAE AMS 4037 : 2014 ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024; -T3 FLAT SHEET, -T351 PLATE) SOLUTION HEAT TREATED
    MIL-PRF-23377 Revision K:2012 PRIMER COATINGS: EPOXY, HIGH-SOLIDS
    SAE AMS 4045 : 2016 ALUMINUM ALLOY SHEET AND PLATE 5.6ZN - 2.5MG - 1.6CU - 0.23CR 7075: (-T6 SHEET, -T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED
    SAE AMS 5516 : 2012 STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 18CR - 9.0NI (SAE 30302), SOLUTION HEAT TREATED
    SAE AS 5127/1 : 2014 AEROSPACE STANDARD TEST METHODS FOR AEROSPACE SEALANTS TWO-COMPONENT SYNTHETIC RUBBER COMPOUNDS
    MIL-DTL-81706 Revision B:2004 Chemical Conversion Materials for Coating Aluminum and Aluminum Alloys
    MIL-DTL-5541 Revision F:2006 Chemical Conversion Coatings on Aluminum and Aluminum Alloys
    SAE AMS P 83310 : 2016 PLASTIC SHEET, POLYCARBONATE, TRANSPARENT
    SAE AMS 3100 : 2013 ADHESION PROMOTER FOR POLYSULFIDE SEALING COMPOUNDS
    SAE AMS 3020 : 2013 OIL, REFERENCE, FOR 'L' STOCK RUBBER TESTING
    MIL-PRF-23699 Revision G:2014 Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Numbers: O-152, O-154, O-156, and O-167
    SAE AMS 2629 : 2017 FLUID, JET REFERENCE
    MIL-PRF-25690 Revision B:1993 PLASTIC, SHEET AND FORMED PARTS, MODIFIED ACRYLIC BASE, MONOLITHIC, CRACK PROPAGATION RESISTANT
    MIL-PRF-83282 Revision D:1997 HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537
    TT-I-735 Revision A:1963 ISOPROPYL ALCOHOL
    SAE AMS 3167 : 2005 SOLVENTS, WIPE FOR CLEANING PRIOR TO APPLICATION OF PRIMER AND TOP COAT MATERIALS, OR SEALING COMPOUNDS
    MIL-PRF-85582 Revision E:2012 PRIMER COATINGS: EPOXY, WATERBORNE
    SAE AMS 2471 : 2014 ANODIC TREATMENT OF ALUMINUM ALLOYS SULFURIC ACID PROCESS, UNDYED COATING
    SAE AMS G 25667 : 2016 GLASS, MONOLITHIC, AIRCRAFT GLAZING
    SAE AMS 4901 : 2015 TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 70.0 KSI (485 MPA)
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