SAE AMS2355M
Current
The latest, up-to-date edition.
QUALITY ASSURANCE, SAMPLING AND TESTING, ALUMINUM ALLOYS AND MAGNESIUM ALLOY, WROUGHT PRODUCTS (EXCEPT FORGING STOCK), AND ROLLED, FORGED, OR FLASH WELDED RINGS
Hardcopy , PDF
English
19-05-2017
1 SCOPE
2 APPLICABLE DOCUMENTS
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 ACKNOWLEDGMENT
7 REJECTIONS
8 NOTES
Specifies quality assurance sampling and testing procedures used to determine conformance to applicable specification requirements of wrought aluminum alloy and wrought magnesium alloy mill products (except forging stock), and includes quality assurance and testing procedures for rolled, forged, and flash welded rings.
Committee |
AMS-D
|
DevelopmentNote |
Supersedes SAE MAM 2355. (01/2008)
|
DocumentType |
Revision
|
Pages |
16
|
PublisherName |
SAE International
|
Status |
Current
|
Supersedes |
SAE AMS4304C:2009(S2022) | Aluminum Alloy, Discontinuously Reinforced Sheet 2009/SiC/15w (T8P) Solution Heat Treated, Stretched, and Precipitation Heat Treated(STABILIZED Nov 2022) |
SAE AMS4478B:2023 | Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024, -T81 Sheet, -T851 Plate) Solution Heat Treated, Cold Worked and Artificially Aged |
SAE AMS4086P | Aluminum Alloy, Drawn, Round, Seamless Hydraulic Tubing 4.4Cu - 1.5Mg - 0.60Mn (2024-T3) Solution Heat Treated, Cold Worked, and Naturally Aged |
SAE AMS4374A:2022 | Aluminum Alloy, Extruded Profiles 8.9Zn - 2.2Cu - 2.2Mg - 0.15Zr (7136-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged |
SAE AMS4613B:2022 | Aluminum Alloy, Sheet and Plate, 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr, Solution Heat Treated, Cold Worked (8%) and Precipitation Heat Treated (2219 -T87) |
SAE AMS4466B:2022 | Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024, -T361 Sheet and Plate) Solution Heat Treated, 6% Cold Worked, and Naturally Aged |
SAE AMS4365A:2022 | Aluminum Alloy, Plate 7.9Zn - 1.2Cu - 2.1Mg - 0.10Zr (7097-T7651) Solution Heat Treated, Stress Relieved, and Overaged |
SAE AMS4458B:2022 | Aluminum Alloy, Plate (2.7 Cu - 1.8 Li - 0.7 Zn) 2099-T86 Solution Heat Treated, Cold Worked, and Artificially Aged |
SAE AMS4371C:2023 | Magnesium Alloy, Plate 4.0Y - 2.25Nd - 0.5Zr (WE43C - T5) Precipitation Heat Treated |
SAE AMS4245G:2023 | Aluminum Alloy, Welding Wire 5.0Si - 1.2Cu - 0.50Mg (C355.0)(NONCURRENT Jan 2008) |
SAE AMS4342G:2023 | Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T74511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged |
SAE AMS4111F | Aluminum Alloy Forgings 7.7Zn - 2.5Mg - 1.5Cu - 0.16Cr (7049-T73) Solution and Precipitation Heat Treated |
SAE AMS4193E | Aluminum Alloy, Sheet, and Plate 4.4Cu - 1.5Mg - 0.60Mn (2024-T861) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated |
SAE AMS4475C:2024 | Aluminum Alloy, Coiled Sheet, Alclad 4.4Cu – 1.5Mg – 0.60Mn (Alclad 2024; -T4 Coiled Sheet) Solution Heat Treated |
SAE AMS4369A:2024 | Aluminum Alloy, Discontinuously Reinforced Extruded Bar, Rod, Wire and Shapes, (2124A/SiC/25p (0.7 µm) (T1P) |
SAE AMS4147E | Aluminum Alloy Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7352) Solution Heat Treated, Stress Relieved by Compression, and Overaged |
SAE AMS4402B:2018(S2024) | Aluminum Alloy, Extruded Profiles (2024-T432) 4.4Cu - 1.5Mg - 0.6Mn Annealed, Stretch Formed, Solution Heat Treated and Stress Relieved by Stretching |
SAE AMS 4063F:2019 | Aluminum Alloy, Clad One Side, Sheet, 1.25Mn - 0.12Cu (No. 11-0 Brazing Sheet), Annealed |
SAE AMS4379A:2024 | Aluminum Alloy, Discontinuously Reinforced Extruded Bar, Rod, Wire and Shapes, 2124A/SiC/25p (3 µm) - T1P |
SAE AMS4401B | Aluminum Alloy, Plate (7140-T7451) 6.6Zn - 1.8Cu - 2.0Mg - 0.10Zr Solution Heat Treated, Stress Relieved, and Overaged |
SAE AMS4204E:2024 | Aluminum Alloy, Plate, 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7651), Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated |
SAE AMS 4172G : 2019 | Aluminum Alloy, Extrusions, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T4511 or T4510), Solution Heat Treated and Stress Relieved by Stretching |
SAE AMS4204D | Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7651) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated |
ASTM E 607 : 2002 | Standard Test Method for Atomic Emission Spectrometric Analysis Aluminum Alloys by the Point to Plane Technique Nitrogen Atmosphere |
ASTM E 466 : 2015 : REDLINE | Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials |
ASTM E 384 : 2017 : REDLINE | Standard Test Method for Microindentation Hardness of Materials |
ASTM B 557 : 2015 : REDLINE | Standard Test Methods for Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products |
ASTM B 953 : 2013 : REDLINE | Standard Practice for Sampling Magnesium and Magnesium Alloys for Spectrochemical Analysis |
ASTM E 10 : 2017-05 | TEST METHOD FOR BRINELL HARDNESS OF METALLIC MATERIALS |
MIL-STD-1537 Revision C:2002 | Electrical Conductivity Test for Verification of Heat Treatment of Aluminum Alloys, Eddy Current Method |
ASTM B 646 : 2017 : REDLINE | Standard Practice for Fracture Toughness Testing of Aluminum Alloys |
SAE ARP 1917 : 2002 | CLARIFICATION OF TERMS USED IN AEROSPACE METALS SPECIFICATIONS |
ASTM E 9 : 2009 | Standard Test Methods of Compression Testing of Metallic Materials at Room Temperature |
ASTM E 716 : 2016 : REDLINE | Standard Practices for Sampling and Sample Preparation of Aluminum and Aluminum Alloys for Determination of Chemical Composition by Spark Atomic Emission Spectrometry |
ASTM E 290 : 2014 : REDLINE | Standard Test Methods for Bend Testing of Material for Ductility |
ASTM E 1004 : 2017 : REDLINE | Standard Test Method for Determining Electrical Conductivity Using the Electromagnetic (Eddy Current) Method |
ASTM B 954 : 2015 : REDLINE | Standard Test Method for Analysis of Magnesium and Magnesium Alloys by Atomic Emission Spectrometry |
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