ARP1110A Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys

Reaffirmed

10/01/2000

Features
Issuing Committee
Scope
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/ARP1110A
Pages
1
Citation
SAE International Recommended Practice, Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys, SAE Standard ARP1110A, Reaffirmed October 2000, Revised May 1994, Issued November 1969, https://doi.org/10.4271/ARP1110A.
Additional Details
Publisher
Published
Oct 1, 2000
Product Code
ARP1110A
Content Type
Recommended Practice
Status
Reaffirmed
Language
English

Revisions