SAE AMS3277J
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Sealing Compound, Polythioether Rubber Fast Curing for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C)
Hardcopy , PDF
12-02-2019
English
02-12-2015
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Specifies polythioether rubber fuel resistant sealing compounds supplied as a two-component system which cures at room temperature.
| DevelopmentNote |
Supersedes MIL S 29574. (09/2005) Supersedes SAE AMS S 29574. (03/2011)
|
| DocumentType |
Standard
|
| Pages |
16
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This specification covers polythioether rubber fuel resistant sealing compounds supplied as a two-component system which cures at room temperature.
| SAE AMS3144 | Primer, Anodic Electrodeposition for Aircraft Applications |
| 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 |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| MIL-HDBK-510 Revision A:2014 | AEROSPACE FUELS CERTIFICATION |
| 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) |
| MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
| NASA MSFC SPEC 3659 : 2012 | PROCESS SPECIFICATION FOR ELECTRICAL BONDING |
| MIL-STD-7179 Revision A:2009 | Finishes, Coatings, and Sealants, for the Protection of Aerospace Weapons Systems and Support Equipment |
| 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 AMSC27725D | Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C) |
| SAE AMS3276F | Sealing Compound, Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C) |
| SAE AMS4911N | Titanium Alloy, Sheet, Strip, and Plate 6Al - 4V Annealed |
| MIL-PRF-85285 Revision E:2012 | COATING: POLYURETHANE, 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 AMS3020A | Oil, Reference, for “L” Stock Rubber Testing |
| SAE AMS2629E | Fluid, Jet Reference |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| 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 |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.