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SAE ARP1110 Rev D

Current Revision

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

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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.

SDO SAE: SAE International
Document Number ARP1110
Publication Date Jan. 21, 2021
Language en - English
Page Count 5
Revision Level D
Supercedes
Committee
Publish Date Document Id Type View
Jan. 21, 2021 ARP1110D Revision
Aug. 10, 2015 ARP1110C Revision
June 23, 2006 ARP1110B Revision
May 1, 1994 ARP1110A Revision
Dec. 1, 1991 ARP1110 Revision