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SAE ARP 823F : 2019

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

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)

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