SAE AMS 3276 : 2016
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 DEGREES F (182 DEGREES C)
02-05-2024
25-10-2016
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.
Committee |
AMS-G9
|
DocumentType |
Standard
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
SAE AMS 3166 : 2014 | SOLVENTS, CLEANING, CLEANING PRIOR TO APPLICATION OF SEALING COMPOUNDS |
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 C 27725 : 2016 | COATING, CORROSION PREVENTATIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS, FOR USE TO 250 DEGREES F (121 DEGREES C) |
SAE AMS 3379 : 2013(R2018) | 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:2022 | 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 AMS 3263 : 1997 | SEALING COMPOUND, POLYTHIOETHER, AMBIENT CURE OR IMMEDIATE HEAT CURE FOR AIRCRAFT STRUCTURES, FUEL RESISTANT WITH INTERMITTENT USE TO 400 MDCF (204 MDCC) |
SAE AMS 3726/2 : 1991 | SHIMS, FILLED RESIN COMPOUND, PRE-CATALYZED SHEET |
SAE AMS 3100 : 2013 | ADHESION PROMOTER FOR POLYSULFIDE SEALING COMPOUNDS |
SAE AS 1301 : 2015 | ADAPTERS - PORT CONNECTION, RING LOCKED DESIGN, INSTALLATION AND REMOVAL OF |
MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
SAE MA 2114 : 2017 | ADAPTER - PORT CONNECTION, RING LOCKED INSTALLATION AND REMOVAL OF |
MIL-DTL-18264 Revision E:2015 | FINISHES, ORGANIC, WEAPONS SYSTEMS, APPLICATION AND CONTROL OF |
SAE AMS 3259 : 1997 | SEALING COMPOUND, POLYTHIOETHER - NONCHROMATED, CORROSION INHIBITING FOR INTERMITTENT USE TO 360 DEGREE F (182 DEGREE C) |
SAE AS 5551 : 2017 | FITTING ASSEMBLY - 24 DEGREES 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 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 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 3092 : 2015 | RELEASE AGENT, FOR USE DURING FORM-IN-PLACE GASKET PREPARATION |
SAE AMS 3167 : 2005 | SOLVENTS, WIPE FOR CLEANING PRIOR TO APPLICATION OF PRIMER AND TOP COAT MATERIALS, OR SEALING COMPOUNDS |
SAE AMS3379A:2013(S2023) | Sealing Compound, Polysulfide Rubber Performed Strips for Sealing Removable Doors, Skins, and Panels(STABILIZED Aug 2023) |
SAE AMS C 27725 : 2016 | COATING, CORROSION PREVENTATIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS, FOR USE TO 250 DEGREES F (121 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 3100 : 2013 | ADHESION PROMOTER FOR POLYSULFIDE SEALING COMPOUNDS |
SAE AMS 3020 : 2013 | OIL, REFERENCE, FOR 'L' STOCK RUBBER TESTING |
SAE AMS 2629 : 2017 | FLUID, JET REFERENCE |
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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