SAE AMS 3277 : 2015
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 DEGREES F (182 DEGREES C)
Hardcopy , PDF
02-12-2019
English
01-01-2015
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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 polythioether rubber fuel resistant sealing compounds supplied as a two-component system which cures at room temperature.
| Committee |
AMS G9
|
| 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Superseded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 |
| SAE AMS 3144 : 2012 | PRIMER, ANODIC ELECTRODEPOSITION FOR AIRCRAFT APPLICATIONS |
| 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 |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| MIL-HDBK-510 Revision A:2014 | AEROSPACE FUELS CERTIFICATION |
| 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) |
| 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 ARP 4118 : 2013 | 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 AMS C 27725 : 2016 | COATING, CORROSION PREVENTATIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS, FOR USE TO 250 DEGREES F (121 DEGREES C) |
| SAE AMS 3276 : 2016 | SEALING COMPOUND, INTEGRAL FUEL TANKS AND GENERAL PURPOSE, INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C) |
| SAE AMS 4911 : 2014 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, 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 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 |
| SAE AMS 3020 : 2013 | OIL, REFERENCE, FOR 'L' STOCK RUBBER TESTING |
| SAE AMS 2629 : 2017 | FLUID, JET REFERENCE |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| SAE AS 5502 : 2016 | STANDARD REQUIREMENTS FOR AEROSPACE SEALANTS AND ADHESION PROMOTERS |
| MIL-PRF-85582 Revision E:2012 | PRIMER COATINGS: EPOXY, WATERBORNE |
| SAE AS 5127 : 2013 | AEROSPACE STANDARD TEST METHODS FOR AEROSPACE SEALANTS METHODS FOR PREPARING AEROSPACE SEALANT TEST SPECIMENS |
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