SAE AMS3276F
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Sealing Compound, Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C)
Published date
16-05-2016
Publisher
Superseded date
02-05-2024
Superseded by
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Specifies fuel-resistant polysulfide (T) sealing compounds supplied as a two-component system.
| DocumentType |
Standard
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This specification covers fuel-resistant polysulfide (T) sealing compounds supplied as a two-component system.
| SAE AMS3166C | Solvents, Cleaning, Cleaning Prior to Application of Sealing Compounds |
| 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 AMSC27725D | Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C) |
| SAE AMS3379 | Sealing Compound, Polysulfide Rubber Preformed Strips for Sealing Removable Doors, Skins, and Panels |
| MIL-DTL-14072 Revision F:2013 | Finishes for Ground Based Electronic Equipment |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| SAE AMS3278C | Sealing and Coating Compound, Polyurethane (PUR) Fuel Resistant, High Tensile Strength/Elongation for Integral Fuel Tanks/Fuel Cavities/General Purpose |
| P-W-2891 Revision A:2002 | Wipe Solvents, Exempt and Non-Exempt |
| MIL-STD-7179 Revision A:2009 | Finishes, Coatings, and Sealants, for the Protection of Aerospace Weapons Systems and Support Equipment |
| MIL-HDBK-510 Revision A:2014 | Aerospace Fuels Certification |
| SAE AMS3263A | Sealing Compound, Polythioether, Ambient Cure or Immediate Heat Cure For Aircraft Structures, Fuel Resistant with Intermittent Use to 400°CF (204°CC) |
| SAE AMS3726/2B | Shims, Filled Resin Compound Precatalyzed Sheet |
| SAE AMS3100D | Adhesion Promoter For Polysulfide Sealing Compounds |
| SAE AS1301F | Adapters - Port Connection, Ring Locked Design, Installation and Removal of |
| MIL-HDBK-510-1 Revision A:2010 | Aerospace Fuels Certification (S/S by MIL-HDBK-510) |
| SAE MA2114B | Adapter - Port Connection, Ring Locked Installation and Removal of |
| MIL-DTL-18264 Revision E:2015 | Finishes, Organic, Weapons Systems, Application and Control of |
| SAE AMS3259B | Sealing Compound, Polythioether Nonchromated, Corrosion Inhibiting for Intermittent Use to 360°F (182°C) |
| SAE AS5551B | Fitting Assembly - 24° Cone Flareless per AS5827, 5080 psi, Port Connection, Port Preparation, Installation and Removal of AS5550 and AS5865 |
| NASA MSFC SPEC 3659 : 2012 | PROCESS SPECIFICATION FOR ELECTRICAL BONDING |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| SAE AMS3277J | Sealing Compound, Polythioether Rubber Fast Curing for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C) |
| SAE ARP4118A | Isolation and Corrosion Protection of Dissimilar Materials, Carbon Composite Structure Repair |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| SAE AMS3092A | Release Agent, for Use During Form-In-Place Gasket Preparation |
| 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 AMS4911N | Titanium Alloy, Sheet, Strip, and Plate 6Al - 4V Annealed |
| MIL-PRF-85285 Revision E:2012 | Topcoat, Aircraft and Support Equipment |
| 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 |
| SAE AMS3100D | Adhesion Promoter For Polysulfide Sealing Compounds |
| SAE AMS3020A | Oil, Reference, for “L” Stock Rubber Testing |
| SAE AMS2629E | Fluid, Jet Reference |
| SAE AS5502D | Standard Requirements for Aerospace Sealants and Adhesion Promoters |
| MIL-PRF-85582 Revision E:2012 | PRIMER COATINGS: EPOXY, WATERBORNE |
| SAE AS5127B | Aerospace Standard Test Methods for Aerospace Sealants Methods for Preparing Aerospace Sealant Test Specimens |
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