SAE ARP1110A-1994
Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys

Standard No.

SAE ARP1110A-1994

Release Date

1994

Published By

Society of Automotive Engineers (SAE)

Status

Withdraw

Replace By

SAE ARP1110A-2000

Latest

SAE ARP1110D-2021

Scope

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. 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.

SAE ARP1110A-1994 history

• 2021 SAE ARP1110D-2021 Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys
• 2015 SAE ARP1110C-2015 Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys
• 2011 SAE ARP1110B-2011 Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys
• 2011 SAE ARP1110-2011 MINIMIZING STRESS CORROSION CRACKING IN HEAT TREATABLE WROUGHT LOW ALLOY AND MARTENSITIC CORROSION RESISTANT STEELS
• 2006 SAE ARP1110B-2006 Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys
• 2000 SAE ARP1110A-2000 Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys
• 1994 SAE ARP1110A-1994 Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys