SAE AMS S 8802 : 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Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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, FUEL RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES
Hardcopy , PDF
08-02-2019
English
01-01-2015
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, two-component polysulfide synthetic rubber compounds which cure at room temperature.
Committee |
AMS G-9
|
DevelopmentNote |
1999 version supersedes MIL S 8802. (03/2003)
|
DocumentType |
Standard
|
Pages |
13
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
Standards | Relationship |
MIL-S-8802 Revision F:1990 | Similar to |
MIL-S-8840 Revision B:1965 | Similar to |
SAE AMS 3116 A : 2005 | PRIMER COATING; EPOXY, CHEMICAL AND SOLVENT RESISTANT NON-CHROMATED, CORROSION PREVENTIVE |
MIL-PRF-32405 Base Document:2013 | CLEANER, HAND WIPE, FOR AVIATION AND MISSILE SYSTEMS, METALLIC SUBSTRATES, LOW OR EXEMPT VOC |
MIL-DTL-27193 Revision D:2017 | INDICATOR, ATTITUDE ARU-2B/A |
SAE AMS 3278 : 2016 | SEALING AND COATING COMPOUND, POLYURETHANE (PUR), FUEL RESISTANT, HIGH TENSILE STRENGTH/ELONGATION, FOR INTEGRAL FUEL TANKS/FUEL CAVITIES/GENERAL PURPOSE |
MIL-DTL-14072 Revision F:2013 | FINISHES FOR GROUND BASED ELECTRONIC EQUIPMENT |
MIL-STD-2003-3 Revision A:2009 | ELECTRIC PLANT INSTALLATION STANDARD METHODS FOR SURFACE SHIPS AND SUBMARINES (PENETRATIONS) |
MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
MIL-HDBK-510 Revision A:2014 | AEROSPACE FUELS CERTIFICATION |
SAE AMS S 83318 : 2016 | SEALING COMPOUND, POLYSULFIDE TYPE, LOW TEMPERATURE CURING, QUICK REPAIR, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES |
SAE AMS 3100 : 2013 | ADHESION PROMOTER FOR POLYSULFIDE SEALING COMPOUNDS |
MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
SAE AMS 3266 : 2017 | SEALING COMPOUND, POLYTHIOETHER ELASTOMERIC TWO-PART ELECTRICALLY CONDUCTIVE |
MIL-PRF-32295 Revision B:2017 | CLEANER, NON-AQUEOUS, LOW-VOC, HAP-FREE |
MIL-PRF-32597 Base Document:2018 | CLEANER, POLYMER AND POLYMER MATRIX COMPOSITE (PMC) MATERIAL, NON-AQUEOUS, HAP-FREE |
MIL-DTL-18264 Revision E:2015 | FINISHES, ORGANIC, WEAPONS SYSTEMS, APPLICATION AND CONTROL OF |
MIL-DTL-287 Revision J:2012 | WAVEGUIDE ASSEMBLIES, FLEXIBLE, TWISTABLE AND NON-TWISTABLE, GENERAL SPECIFICATION FOR |
NFPA 1150 : 2017 | FOAM CHEMICALS FOR FIRES IN CLASS A FUELS |
NASA MSFC SPEC 3659 : 2012 | PROCESS SPECIFICATION FOR ELECTRICAL BONDING |
NASA MSFC HDBK 3697 : 2014 | ELECTRICAL BONDING DESIGN GUIDE HANDBOOK |
SAE AMS S 4383 : 2015 | SEALING COMPOUND, TOPCOAT, FUEL TANK BUNA-N TYPE |
MIL-STD-7179 Revision A:2009 | Finishes, Coatings, and Sealants, for the Protection of Aerospace Weapons Systems and Support Equipment |
MIL-DTL-58085 Revision C:2012 | Light, Beacon, Anti-Collision, Aircraft |
MIL-STD-171 Revision F:2011 | FINISHING OF METAL AND WOOD SURFACES |
SAE J 2270 : 2016 | SHIP SYSTEMS AND EQUIPMENT - THREADED FASTENERS - INSPECTION, TEST, AND INSTALLATION GUIDANCE |
SAE AS 50881 : 2015 | WIRING AEROSPACE VEHICLE |
MIL-PRF-87937 Revision D:2001 | CLEANING COMPOUND, AEROSPACE EQUIPMENT |
SAE AMS 3144 : 2012 | PRIMER, ANODIC ELECTRODEPOSITION FOR AIRCRAFT APPLICATIONS |
MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
SAE ARP 4118 : 2013 | ISOLATION AND CORROSION PROTECTION OF DISSIMILAR MATERIALS, CARBON COMPOSITE STRUCTURE REPAIR |
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-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 |
MIL-DTL-81706 Revision B:2004 | Chemical Conversion Materials for Coating Aluminum and Aluminum Alloys |
SAE AMS 3100 : 2013 | ADHESION PROMOTER FOR POLYSULFIDE SEALING COMPOUNDS |
SAE AMS 2629 : 2017 | FLUID, JET REFERENCE |
SAE AS 5502 : 2016 | STANDARD REQUIREMENTS FOR AEROSPACE SEALANTS AND ADHESION PROMOTERS |
SAE AS 5127 : 2013 | AEROSPACE STANDARD TEST METHODS FOR AEROSPACE SEALANTS METHODS FOR PREPARING AEROSPACE SEALANT TEST SPECIMENS |
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