SAE ARP823F
Current
The latest, up-to-date edition.
Minimizing Stress-Corrosion Cracking in Wrought High-Strength Aluminum Alloy Products
Hardcopy , PDF
English
17-04-2019
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.
| DocumentType |
Standard
|
| Pages |
5
|
| ProductNote |
THIS STANDARD ALSO REFERS TO NBS Monograph 156.
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
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.
| SAE AMS4374A | 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 | 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 | 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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