SAE AMS4037Q
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024; -T3 FLAT SHEET, -T351 PLATE) SOLUTION HEAT TREATED
Hardcopy , PDF
24-08-2020
English
01-01-2014
1 SCOPE
2 APPLICABLE DOCUMENTS
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 ACKNOWLEDGEMENT
7 REJECTIONS
8 NOTES
This specification covers an aluminum alloy in the form of sheet and plate from 0.008 to 4.000 inches (0.20 to 101.60 mm) in thickness, inclusive (See 8.4).
Committee |
AMS D
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DevelopmentNote |
Supersedes SAE AMS 4033 (07/1999)
|
DocumentType |
Standard
|
Pages |
5
|
PublisherName |
SAE International
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Status |
Superseded
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SupersededBy | |
Supersedes |
SAE AMS2482E | HARD ANODIC COATING ON ALUMINUM ALLOYS POLYTETRAFLUOROETHYLENE (PTFE)-IMPREGNATED OR CODEPOSITED |
SAE AMS 3116 A : 2005 | PRIMER COATING; EPOXY, CHEMICAL AND SOLVENT RESISTANT NON-CHROMATED, CORROSION PREVENTIVE |
SAE AMS1630C | CLEANER, CARPET SHAMPOO TYPE |
SAE ARP 5485 : 2017 | ENDURANCE TIME TEST PROCEDURES FOR SAE TYPE 2/3/4 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
SAE AS5127B | AEROSPACE STANDARD TEST METHODS FOR AEROSPACE SEALANTS METHODS FOR PREPARING AEROSPACE SEALANT TEST SPECIMENS |
SAE AMS 3695 : 2014 | ADHESIVE FILM, EPOXY-BASE, FOR HIGH DURABILITY STRUCTURAL ADHESIVE BONDING |
SAE AMS1428J | FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN, (PSEUDOPLASTIC), SAE TYPES 2, 3 AND 4 |
SAE AMS1435C | FLUID, GENERIC, DEICING/ANTI-ICING, RUNWAYS AND TAXIWAYS |
SAE AMS2514A | ANODIC COATING ON ALUMINUM ALLOYS, SULFURIC ACID PROCESS, RESIN-SEALED |
SAE AMS1536B | CLEANER FOR AIRCRAFT COMPONENTS COLD TANK TYPE, SOLVENT-BASE |
SAE AMS3255B | SEALING TAPE, SHEET, OR GASKET, POLYTETRAFLUOROETHYLENE, EXPANDED (EPTFE) OIL AND WATER RESISTANT |
SAE AMS 3117 : 2011 | PRIMER ZINC MOLYBDATE |
SAE AMS 3107 : 1983(R2014) | PRIMER, ADHESIVE, CORROSION-INHIBITING, FOR HIGH DURABILITY STRUCTURAL ADHESIVE BONDING |
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 AMS1374A | REMOVER, POLYURETHANE/EPOXY PAINT, ALKALINE, HOT-TANK TYPE |
SAE ARP 1675 : 2014 | STRUCTURAL WELDBONDING OF ALUMINUM STRUCTURES |
SAE AMS3259B | SEALING COMPOUND, POLYTHIOETHER - NONCHROMATED, CORROSION INHIBITING FOR INTERMITTENT USE TO 360 DEGREE F (182 DEGREE C) |
SAE AMS 3688 : 2014 | ADHESIVE, FOAMING, HONEYCOMB CORE SPLICE, STRUCTURAL, -55 DEGREES C TO +82 DEGREES C (-65 DEGREES F TO +180 DEGREES F) |
SAE AMS 3689 : 2014 | ADHESIVE, FOAMING, HONEYCOMB, CORE SPLICE, STRUCTURAL, -54 TO +177 DEGREES C (-65 TO +350 DEGREES F) |
SAE AMS 3075 : 2016 | COMPOUND, CORROSION-PREVENTIVE HARD FILM, HOT APPLICATION |
SAE AMS2472G | ANODIC TREATMENT OF ALUMINUM ALLOYS, SULFURIC ACID PROCESS, DYED COATING |
SAE AMS 1453 : 2015 | DISINFECTANT CLEANER FOR AIRCRAFT INTERIOR GENERAL PURPOSE LIQUID |
MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
SAE AMS 2483 : 2015 | BLACKENING SOLUTION FOR ALUMINUM, TOUCH-UP SOLUTION |
MIL-DTL-7034 Revision F:2005 | PULLEYS, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
BS M 75:1994 | Aircraft de-icing/anti-icing Newtonian fluids, ISO type I |
MIL P 7034 : D | PULLEY, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT |
SAE AMS4254C | ALUMINUM ALLOY, ARAMID FIBER REINFORCED, LAMINATED SHEET, 4.4CU - 1.5MG - 0.6MN (2024-T3), 3, 5, 7, OR 9 PLY |
SAE AMS3077 | COMPOUND, CORROSION PREVENTIVE Soft Film, Thixotropic, Cold Application- |
SAE AMS1424N | FLUID, AIRCRAFT DEICING/ANTI-ICING, SAE TYPE 1 |
SAE ARP 5945 : 2017 | ENDURANCE TIME TEST PROCEDURES FOR SAE TYPE 1 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
SAE AMS1548B | CLEANER, TURBINE ENGINE GAS PATH, SOLVENT EMULSION TYPE |
SAE AMS3054C | OIL, LUBRICATING, LOW TEMPERATURE FOR -55 DEGREES C (-67 DEGREES F) SERVICE |
SAE AMS 1377 : 2012 | REMOVER, PAINT, EPOXY AND POLYURETHANE PAINT SYSTEM, NON-CHLORINATED SOLVENT |
SAE AMSP5315B | ACRYLONITRILE-BUTADIENE (NBR) RUBBER FOR FUEL-RESISTANT SEALS 60 TO 70 |
SAE ARP1862A | CLEANING EFFICIENCY OF TURBINE ENGINE GAS PATH CLEANERS, LABORATORY TEST METHOD |
SAE AS 5901 : 2014 | WATER SPRAY AND HIGH HUMIDITY ENDURANCE TEST METHODS FOR SAE AMS1424 AND SAE AMS1428 AIRCRAFT DEICING/ANTI-ICING FLUIDS |
BS M 78:1995 | Aircraft de-icing/anti-icing non-Newtonian fluids, ISO type II |
SAE AMS1426D | FLUID, DEICING/ANTI-ICING, RUNWAYS AND TAXIWAYS GLYCOL BASE |
MIL-DTL-5541 Revision F:2006 | Chemical Conversion Coatings on Aluminum and Aluminum Alloys |
SAE AMS 1375 : 2012 | REMOVER, PAINT, EPOXY AND POLYURETHANE PAINT SYSTEMS |
SAE AMS1376B | REMOVER, EPOXY PAINT, ACID TYPE, THICKENED |
SAE AMS2469J | HARD ANODIC COATING ON ALUMINUM AND ALUMINUM ALLOYS |
SAE AMS 1388 : 2008 | REMOVER, TEMPORARY COATING, ALKALINE TYPE, WATER BASE |
SAE AMS1540C | CLEANER, THRUST REVERSER, WATER-BASE |
SAE ARP 1755 : 2000 | EFFECT OF CLEANING AGENTS ON AIRCRAFT ENGINE MATERIALS, STOCK LOSS TEST METHOD |
SAE AMS 7258 : 2001 | RINGS, SEALING, BUTADIENE-ACRYLONITRILE (NBR) RUBBER FUEL RESISTANT, LOW SHRINKAGE 65-75 |
SAE AMS 1432 : 1995 | FLUID, DEICING/ANTI-ICING, RUNWAYS AND TAXIWAYS, POTASSIUM ACETATE BASE |
SAE AMS1431D | COMPOUND, SOLID RUNWAY AND TAXIWAY DEICING/ANTI-ICING |
SAE AMS2471H | ANODIC TREATMENT OF ALUMINUM ALLOYS SULFURIC ACID PROCESS, UNDYED COATING |
SAE AMS 3686 : 2014 | ADHESIVE, POLYIMIDE RESIN, FILM AND PASTE HIGH TEMPERATURE RESISTANT, 315 DEGREES C (599 DEGREES F) |
SAE AMS1659 | COATING, SOIL BARRIER Semi-Permanent |
MIL-DTL-81706 Revision B:2004 | Chemical Conversion Materials for Coating Aluminum and Aluminum Alloys |
SAE AMS3095A | PAINT: HIGH GLOSS FOR AIRLINE EXTERIOR SYSTEM |
SAE AMS2473H | CHEMICAL FILM TREATMENT FOR ALUMINUM ALLOYS, GENERAL PURPOSE COATING |
SAE AMS 1527 : 2014 | CLEANER FOR AIRCRAFT EXTERIOR SURFACES, WATER-MISCIBLE, FOAM-ON, PRESSURE-SPRAYING |
SAE AMS2470N | ANODIC TREATMENT OF ALUMINUM ALLOYS, CHROMIC ACID PROCESS |
SAE AS269J | IDENTIFICATION OF MATERIAL FOR AN, MS AND AS ENGINE AND PROPELLER STANDARD UTILITY PARTS AND ALSO FOR COMPANY PARTS |
SAE AMS3159G | LEAK TEST SOLUTION - LIQUID OXYGEN COMPATIBLE |
SAE AMS3529B | PLASTIC SHEET AND FILM, VINYL COPOLYMERS, UNPLASTICIZED |
SAE AMS3377A | SEALING COMPOUND, ELECTRICALLY CONDUCTIVE CORROSION INHIBITING |
SAE AMS3167B | SOLVENTS, WIPE FOR CLEANING PRIOR TO APPLICATION OF PRIMER AND TOP COAT MATERIALS, OR SEALING COMPOUNDS |
SAE AMS1631C | CLEANER, CARPET WATER EXTRACTION TYPE |
ANSI H35.2 : 2017 | DIMENSIONAL TOLERANCES FOR ALUMINUM MILL PRODUCTS |
ASTM B 666/B666M : 2015 : REDLINE | Standard Practice for Identification Marking of Aluminum and Magnesium Products |
SAE AMS 2772 : 2016 | HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS |
SAE AS1990D | ALUMINUM ALLOY TEMPERS |
SAE AMS2355L | QUALITY ASSURANCE, SAMPLING AND TESTING, ALUMINUM ALLOYS AND MAGNESIUM ALLOY, WROUGHT PRODUCTS (EXCEPT FORGING STOCK), AND ROLLED, FORGED, OR FLASH WELDED RINGS |
ASTM B 660 : 2015 : REDLINE | Standard Practices for Packaging/Packing of Aluminum and Magnesium Products |
ANSI H35.2M : 2013 | DIMENSIONAL TOLERANCES FOR ALUMINUM MILL PRODUCTS (METRIC) |
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