SAE AMS3265E
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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, POLYSULFIDE (T) RUBBER, FUEL RESISTANT, NON-CHROMATED CORROSION INHIBITING, FOR INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C)
Hardcopy , PDF
12-09-2020
English
02-12-2015
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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 polysulfide rubber sealing compounds containing only non-chromated corrosion inhibitors, supplied as a two component system which cures at room temperature.
| Committee |
AMS-G9
|
| DevelopmentNote |
Supersedes MIL S 38228. (04/2014)
|
| DocumentType |
Standard
|
| Pages |
15
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| 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 |
| MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| SAE ARP4118A | ISOLATION AND CORROSION PROTECTION OF DISSIMILAR MATERIALS, CARBON COMPOSITE STRUCTURE REPAIR |
| SAE AMSC27725D | COATING, CORROSION PREVENTATIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS, FOR USE TO 250 DEGREES F (121 DEGREES 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 |
| MIL-PRF-81733 Revision D:1998 | SEALING AND COATING COMPOUND, CORROSION INHIBITIVE |
| SAE AMS3276F | SEALING COMPOUND, INTEGRAL FUEL TANKS AND GENERAL PURPOSE, INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C) |
| SAE AMS4911N | 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 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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