Browse Standards ARP823A
Historical REVISED 1966-09-01

Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products ARP823A

The purpose of this recommended practice is to provide the aerospace industry with recommendations concerning minimizing of stress-corrosion cracking (SCC) in wrought high-strength aluminum alloy products. The detailed recommendations are based on practical engineering experience and reflect those design practices and fabricating procedures which have been found to be most effective in minimizing stress-corrosion cracking in wrought high-strength aluminum alloy products. This ARP provides general guidelines. For further information see references in 4.3.
ARP823E
2013-05-29
Latest
Reaffirmed
ARP823D
1997-03-01
Historical
Reaffirmed
ARP823C
1988-10-01
Historical
Revised
ARP823B
1982-07-01
Historical
Revised
ARP823A
1966-09-01
Historical
Revised
ARP823
1964-01-01
Historical
Issued

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