SAE AMS 3077 A : 1994(S2018)
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
COMPOUND, CORROSION PREVENTIVE, SOFT FILM, THIXOTROPIC, COLD APPLICATION
Hardcopy , PDF
06-05-2018
English
24-04-2018
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
This specification covers a ready-mixed thixotropic compound in the form of a stable film-forming compound suitable for application by brushing or spraying.
Committee |
AMS-J
|
DocumentType |
Standard
|
Pages |
15
|
PublisherName |
SAE International
|
Status |
Superseded
|
Supersedes |
SAE AMS2473H | CHEMICAL FILM TREATMENT FOR ALUMINUM ALLOYS, GENERAL PURPOSE COATING |
TT-N-95 Revision B:1967 | |
O-N-350 Revision C:1991 | NITRIC ACID, TECHNICAL |
MIL C 16173 : E | CORROSION PREVENTIVE COMPOUND, SOLVENT CUTBACK, COLD APPLICATION |
SAE AMS 4049 : 2016 | 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 |
SAE AMS2475G | PROTECTIVE TREATMENTS, MAGNESIUM ALLOYS |
AN 960 : 0021 | WASHER, FLAT |
SAE AMS 2820 : 2001 | AEROSOL PACKAGING |
SAE AMS 4376 : 2011(R2018) | PLATE, MAGNESIUM ALLOY - 3.0AL - 1.0ZN - 0.20MN (AZ31B-H26) COLD ROLLED AND PARTIALLY ANNEALED |
MIL-STD-290 Revision H:2013 | PACKAGING AND MARKING OF PETROLEUM AND RELATED PRODUCTS |
SAE AMS 4037 : 2014 | ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024; -T3 FLAT SHEET, -T351 PLATE) SOLUTION HEAT TREATED |
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 |
NAS6403-6420:2002 | BOLT, TENSION, HEX HEAD, CLOSE TOLERANCE, 6AL-4V TITANIUM ALLOY, SHORT THREAD, REDUCED MAJOR THREAD DIAMETER, SELF-LOCKING AND NONLOCKING, 160 KSI FTU |
ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
MIL P 23377 : G | PRIMER COATING, EPOXY, HIGH SOLIDS |
O-T-620 Revision C:1967 | TRICHLOROETHANE-1,1,1, TECHNICAL, INHIBITED (METHYL CHLOROFORM) |
SAE AMS 1425 : 1990 | DEICING FLUID, AIRCRAFT, ETHYLENE GLYCOL BASE |
NAS6303-6320:2016 | BOLT, TENSION, HEX HEAD, CLOSE TOLERANCE, A286 CRES, SHORT THREAD, REDUCED MAJOR THREAD DIA., SELF-LOCKING AND NONLOCKING, 160 KSI FTU |
O-S-598 Revision B:1975 | SODIUM HYDROXIDE, TECHNICAL |
SAE AMS 2350 : 1989 | STANDARDS AND TEST METHODS |
SAE AMS 1526 : 2008 | CLEANER FOR AIRCRAFT EXTERIOR SURFACES, WATER-MISCIBLE, PRESSURE-SPRAYING TYPE |
SAE ARP 1511 : B | CORROSION OF LOW-EMBRITTLING CADMIUM PLATE BY AIRCRAFT MAINTENANCE CHEMICALS |
SAE AMS 2825 : 1987 | MATERIAL SAFETY DATA SHEETS |
SAE AMS5040N | Steel, Sheet and Strip 0.15 Carbon, Maximum Deep Forming Grade |
SAE AMS 4165 : 2013 | ALUMINUM ALLOY, EXTRUSIONS, 4.4CU - 1.5MG - 0.60MN (2024-T3511), SOLUTION HEAT TREATED, STRESS-RELIEVED BY STRETCHING, AND STRAIGHTENED |
NAS1303-1320:2001 | BOLT, TENSION, HEXAGON HEAD 160 KSI FTU |
O-H-765 Revision E:1990 | HYDROCHLORIC ACID, TECHNICAL |
SAE AMS 3808 : 2015 | TAPE, ADHESIVE, PRESSURE-SENSITIVE MASKING |
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