SAE AS 5127/1 : 2014
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
AEROSPACE STANDARD TEST METHODS FOR AEROSPACE SEALANTS TWO-COMPONENT SYNTHETIC RUBBER COMPOUNDS
Hardcopy , PDF
21-03-2020
English
01-01-2014
1. SCOPE
2. REFERENCES
3. CLASSIFICATION
4. PREPARATION OF SEALING COMPOUND
5. APPLICATION PROPERTIES TEST METHODS
6. PERFORMANCE PROPERTIES TEST METHODS
7. RESISTANCE TO HYDROCARBONS
8. PEEL STRENGTH PROPERTIES
9. STORAGE STABILITY
10. NOTES
Defines test methods to determine the application and performance properties of two-component sealing compounds.
Committee |
AMS G9
|
DevelopmentNote |
To be read in conjunction with SAE AS 5127. (05/2002)
|
DocumentType |
Test Method
|
Pages |
44
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
SAE AMS S 83318 : 2016 | SEALING COMPOUND, POLYSULFIDE TYPE, LOW TEMPERATURE CURING, QUICK REPAIR, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES |
SAE AMS 3374 : 2013 | SEALING COMPOUND AIRCRAFT FIREWALL, SILICONE |
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 3255 : 2017 | SEALING TAPE, SHEET, OR GASKET, POLYTETRAFLUOROETHYLENE, EXPANDED (EPTFE) OIL AND WATER RESISTANT |
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) |
MIL-HDBK-510 Revision A:2014 | AEROSPACE FUELS CERTIFICATION |
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 AS 5127 : 2013 | AEROSPACE STANDARD TEST METHODS FOR AEROSPACE SEALANTS METHODS FOR PREPARING AEROSPACE SEALANT TEST SPECIMENS |
SAE AS 81550A : 2014 | INSULATING COMPOUND, ELECTRICAL, EMBEDDING, REVERSION RESISTANT SILICONE |
SAE AMS 3100 : 2013 | ADHESION PROMOTER FOR POLYSULFIDE SEALING COMPOUNDS |
MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
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 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 S 8802 : 2015 | SEALING COMPOUND, FUEL RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES |
SAE AMS 3381 : 2014 | SEALING COMPOUND, AIRCRAFT FIREWALL, NON-SILICONE |
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 3376 : 2015 | SEALING COMPOUND, NON-CURING, FLUOROSILICONE GROOVE INJECTION TEMPERATURE AND FUEL RESISTANT |
SAE AMS 3284 : 2017 | SEALING COMPOUND, LOW ADHESION, FOR REMOVABLE PANELS AND FUEL TANK INSPECTION PLATES |
SAE AMS 3144 : 2012 | PRIMER, ANODIC ELECTRODEPOSITION FOR AIRCRAFT APPLICATIONS |
SAE AMS 3379 : 2013(R2018) | SEALING COMPOUND, POLYSULFIDE RUBBER PREFORMED STRIPS FOR SEALING REMOVABLE DOORS, SKINS, AND PANELS |
SAE AMS 3167 : 2005 | SOLVENTS, WIPE FOR CLEANING PRIOR TO APPLICATION OF PRIMER AND TOP COAT MATERIALS, OR SEALING COMPOUNDS |
SAE AMS3379A:2013(S2023) | Sealing Compound, Polysulfide Rubber Performed Strips for Sealing Removable Doors, Skins, and Panels(STABILIZED Aug 2023) |
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 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 |
ASTM G 85 : 2011 : REDLINE | Standard Practice for Modified Salt Spray (Fog) Testing |
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 |
ASTM D 792 : 2013 : REDLINE | Standard Test Methods for Density and Specific Gravity (Relative Density) of Plastics by Displacement |
SAE AMS P 83310 : 2016 | PLASTIC SHEET, POLYCARBONATE, TRANSPARENT |
ASTM E 11 : 2017 : REDLINE | Standard Specification for Woven Wire Test Sieve Cloth and Test Sieves |
SAE AMS 2629 : 2017 | FLUID, JET REFERENCE |
ASTM G 155 : 2013 : REDLINE | Standard Practice for Operating Xenon Arc Light Apparatus for Exposure of Non-Metallic Materials |
MIL-PRF-25690 Revision B:1993 | PLASTIC, SHEET AND FORMED PARTS, MODIFIED ACRYLIC BASE, MONOLITHIC, CRACK PROPAGATION RESISTANT |
SAE AMS 3333 : 2012 | SEALING COMPOUND, POLYSULFIDE, FOR AIRCRAFT WINDSHIELDS AND CANOPIES, FOR USE UP TO 280 DEGREES F (121 DEGREES C) |
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 AS 5127 : 2013 | AEROSPACE STANDARD TEST METHODS FOR AEROSPACE SEALANTS METHODS FOR PREPARING AEROSPACE SEALANT TEST SPECIMENS |
ASTM D 3359 : 2017 : REDLINE | Standard Test Methods for Rating Adhesion by Tape Test |
SAE AMS G 25667 : 2016 | GLASS, MONOLITHIC, AIRCRAFT GLAZING |
ASTM D 329 : 2007 | Standard Specification for Acetone |
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