Browse Standards ARP1110B
Historical REAFFIRMED 2011-04-12

Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys ARP1110B

The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide the aerospace industry with recommendations concerning the minimization of stress corrosion cracking in wrought heat-treatable carbon and low alloy steels and in austenitic, precipitation hardenable, and martensitic corrosion-resistant steels and alloys.
The detailed recommendations are based on laboratory and field experience and reflect those design practices and fabrication procedures which should avoid in-service stress corrosion cracking.
ARP1110D
2021-01-21
Latest
Revised
ARP1110C
2015-08-10
Historical
Revised
ARP1110
2011-08-10
Historical
Reaffirmed
ARP1110B
2011-04-12
Historical
Reaffirmed
ARP1110A
2000-10-01
Historical
Reaffirmed

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