SAE ARP823F
Current
Current
The latest, up-to-date edition.
Minimizing Stress-Corrosion Cracking in Wrought High-Strength Aluminum Alloy Products
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
17-04-2019
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.The purpose of this recommended practice is to provide the aerospace industry with recommendations concerning minimizing stress corrosion cracking (SCC) in wrought high strength aluminum alloy products.
| Committee |
AMS D
|
| DocumentType |
Revision
|
| Pages |
5
|
| ProductNote |
THIS STANDARD ALSO REFERS TO NBS Monograph 156.
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| 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 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 |
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