SAE AS5127B
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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
17-11-2018
30-05-2013
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.
| DocumentType |
Standard
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| PublisherName |
SAE International
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| Status |
Superseded
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| Supersedes |
This standard describes the accepted methods used for preparing aerospace sealant test specimens for qualification and quality conformance or acceptance testing. AS5127/1 and AS5127/2 are to be used in conjunction with this document and the applicable AMS specifications.
| SAE AS5127/2B | Test Method for Aerospace Firewall Sealant Flame Penetration |
| 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 AMS3265E | Sealing Compound, Polysulfide (T) Rubber, Fuel Resistant, Non-Chromated Corrosion Inhibiting For Intermittent Use to 360 °F (182 °C) |
| SAE AMS3278B | Sealing and Coating Compound, Polyurethane (PUR) Fuel Resistant High Tensile Strength / Elongation For Integral Fuel Tanks / Fuel Cavities / General Purpose |
| SAE AMS3379 | Sealing Compound, Polysulfide Rubber Preformed Strips for Sealing Removable Doors, Skins, and Panels |
| 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 AMSS83318C | Sealing Compound, Polysulfide Type, Low Temperature Curing, Quick Repair, Integral Fuel Tanks and Fuel Cell Cavities |
| SAE AMS3100D | Adhesion Promoter For Polysulfide Sealing Compounds |
| SAE AMSS8802D | Sealing Compound, Fuel Resistant, Integral Fuel Tanks and Fuel Cell Cavities |
| SAE AS81550A | Insulating Compound, Electrical, Embedding, Reversion Resistant Silicone |
| SAE AMS3376C | Sealing Compound, Non-Curing, Fluorosilicone Groove Injection Temperature and Fuel Resistant |
| SAE AMS3255B | Sealing Tape, Sheet, or Gasket, Polytetrafluoroethylene, Expanded (EPTFE) Oil and Water Resistant |
| SAE AMSS4383B | Sealing Compound, Topcoat, Fuel Tank Buna-N Type |
| SAE AMS3266A | Sealing Compound, Polythioether Elastomeric Two-Part Electrically Conductive |
| SAE AMS3381 | Sealing Compound, Aircraft Firewall, Non-Silicone |
| SAE AS5127/1C | Aerospace Standard Test Methods for Aerospace Sealants Two-Component Synthetic Rubber Compounds |
| SAE AMS3167B | Solvents, Wipe for Cleaning Prior to Application of Primer and Top Coat Materials, or Sealing Compounds |
| SAE AMS3374D | Sealing Compound Aircraft Firewall, Silicone |
| SAE AMS3277J | Sealing Compound, Polythioether Rubber Fast Curing for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C) |
| SAE AMS3284C | Sealing Compound, Low Adhesion, for Removable Panels and Fuel Tank Inspection Plates |
| 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 AS5127/2B | Test Method for Aerospace Firewall Sealant Flame Penetration |
| 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 |
| SAE AMS4037Q | 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 AMS4045L | Aluminum Alloy Sheet and Plate 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr 7075: (-T6 Sheet, -T651 Plate) Solution and Precipitation Heat Treated |
| SAE AMS5516P | Steel, Corrosion-Resistant, Sheet, Strip, and Plate 18Cr - 9.0Ni (SAE 30302) Solution Heat Treated |
| SAE AS5127/1C | 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 AMSP83310A | Plastic Sheet, Polycarbonate, Transparent |
| SAE AMS3100D | Adhesion Promoter For Polysulfide Sealing Compounds |
| SAE AMS3020A | 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 AMS2629E | 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 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 AMSG25667A | Glass, Monolithic, Aircraft Glazing |
| SAE AMS4901T | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa) |
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