SAE AS 5127 : 2013
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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
Superseded date
11-17-2018
Superseded by
Published date
01-01-2013
Publisher
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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
Describes the accepted methods used for preparing aerospace sealant test specimens for qualification and quality conformance or acceptance testing.
| Committee |
AMS G9
|
| DocumentType |
Standard
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| 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 |
| 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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