SAE AS5127/1C
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 Two-Component Synthetic Rubber Compounds
Hardcopy , PDF
21-03-2020
English
08-10-2014
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.
DevelopmentNote |
To be read in conjunction with SAE AS 5127. (05/2002)
|
DocumentType |
Standard
|
Pages |
44
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
This SAE Aerospace Standard (AS) describes test methods to determine the application and performance properties of two-component sealing compounds. It shall be used in conjunction with AS5127 and the applicable material specification. When modifications to these test methods are called out in material specifications, the material specification shall take precedence.
SAE AMSS83318C | Sealing Compound, Polysulfide Type, Low Temperature Curing, Quick Repair, Integral Fuel Tanks and Fuel Cell Cavities |
SAE AMS3374D | Sealing Compound Aircraft Firewall, Silicone |
SAE AMS3278B | Sealing and Coating Compound, Polyurethane (PUR) Fuel Resistant High Tensile Strength / Elongation For Integral Fuel Tanks / Fuel Cavities / General Purpose |
SAE AMS3255B | Sealing Tape, Sheet, or Gasket, Polytetrafluoroethylene, Expanded (EPTFE) Oil and Water Resistant |
SAE AMS3265E | Sealing Compound, Polysulfide (T) Rubber, Fuel Resistant, Non-Chromated Corrosion Inhibiting For Intermittent Use to 360 °F (182 °C) |
MIL-HDBK-510 Revision A:2014 | AEROSPACE FUELS CERTIFICATION |
SAE AMS3276F | Sealing Compound, Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C) |
SAE AMS3102 | Sealing Compound, Polythioether Rubber Fast Curing, Light Weight (Specific Gravity 0.78, max.) for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C) |
SAE AS5127B | Aerospace Standard Test Methods for Aerospace Sealants Methods for Preparing Aerospace Sealant Test Specimens |
SAE AS81550A | Insulating Compound, Electrical, Embedding, Reversion Resistant Silicone |
SAE AMS3100D | Adhesion Promoter For Polysulfide Sealing Compounds |
MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
SAE AMS3277J | Sealing Compound, Polythioether Rubber Fast Curing for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C) |
SAE AMSS4383B | Sealing Compound, Topcoat, Fuel Tank Buna-N Type |
SAE AMS3266A | Sealing Compound, Polythioether Elastomeric Two-Part Electrically Conductive |
SAE AMSS8802D | Sealing Compound, Fuel Resistant, Integral Fuel Tanks and Fuel Cell Cavities |
SAE AMS3381 | Sealing Compound, Aircraft Firewall, Non-Silicone |
SAE AMS3281F | Sealing Compound, Polysulfide (T) Synthetic Rubber for Integral Fuel Tank and Fuel Cell Cavities Low Density for Intermittent Use to 360 °F (182 °C) |
SAE AMS3376C | Sealing Compound, Non-Curing, Fluorosilicone Groove Injection Temperature and Fuel Resistant |
SAE AMS3284C | Sealing Compound, Low Adhesion, for Removable Panels and Fuel Tank Inspection Plates |
SAE AMS3144 | Primer, Anodic Electrodeposition for Aircraft Applications |
SAE AMS3379 | Sealing Compound, Polysulfide Rubber Preformed Strips for Sealing Removable Doors, Skins, and Panels |
SAE AMS3167B | Solvents, Wipe for Cleaning Prior to Application of Primer and Top Coat Materials, or Sealing Compounds |
SAE AMS3379A | Sealing Compound, Polysulfide Rubber Performed Strips for Sealing Removable Doors, Skins, and Panels |
SAE AMSC27725D | Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C) |
SAE AMS4049M | 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 AMS4911N | Titanium Alloy, Sheet, Strip, and Plate 6Al - 4V Annealed |
SAE AMS3819C | 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 AMS4045L | 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 AMSP83310A | Plastic Sheet, Polycarbonate, Transparent |
ASTM E 11 : 2017 : REDLINE | Standard Specification for Woven Wire Test Sieve Cloth and Test Sieves |
SAE AMS2629E | 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 AMS3333B | Sealing Compound, Polysulfide For Aircraft Windshields and Canopies, For Use up to 250 °F (121 °C) |
SAE AMS3167B | 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 AMS2471H | Anodic Treatment of Aluminum Alloys Sulfuric Acid Process, Undyed Coating |
SAE AS5127B | 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 AMSG25667A | Glass, Monolithic, Aircraft Glazing |
ASTM D 329 : 2007 | Standard Specification for Acetone |
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