Browse Standards ARP1110C
Current REVISED 2015-08-10

Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys ARP1110C

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.
ARP1110C
2015-08-10
Latest
Revised
ARP1110
2011-08-10
Historical
Reaffirmed
ARP1110B
2011-04-12
Historical
Reaffirmed
ARP1110A
2000-10-01
Historical
Reaffirmed

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