SAE ARP823F
Current
Minimizing Stress-Corrosion Cracking in Wrought High-Strength Aluminum Alloy Products
Hardcopy , PDF
English
04-17-2019
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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