SAE ARP1110D:2021
Current
The latest, up-to-date edition.
Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys
Hardcopy , PDF
English
21-01-2021
Important note : Users cannot be edited or removed once added to your Multi user PDF.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.
| Committee |
AMS E
|
| DocumentType |
Revision
|
| Pages |
5
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| SAE AMS6415V:2022 | Steel, Bars, Forgings, Mechanical Tubing, and Forging Stock 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) |
| SAE AMS5529L:2024 | Steel, Corrosion-Resistant, Sheet and Strip 17Cr - 7.1Ni - 1.1Al (Alloy 17-7) Solution Heat Treated and Cold Rolled, Precipitation Hardenable |
| SAE AMS6499C:2024 | Steel, Bars, Forgings, Mechanical Tubing and Forging Stock, 2.7Si - 0.85Cr - 1.8Ni - 0.4Mo - 0.2V - (0.37 - 0.44C) Premium Aircraft Quality, Double Vacuum Melted |
| SAE AMS6411K:2023 | Steel Bars, Forgings, Mechanical Tubing and Forging Stock 0.88Cr - 1.8Ni - 0.42Mo - 0.08V (0.28 - 0.33C) (4330 Mod) Consumable Electrode Remelted |
| SAE AMS6427P:2023 | Steel Bars, Forgings, Mechanical Tubing, and Forging Stock, Aircraft Quality, 0.88Cr - 1.8Ni - 0.42Mo - 0.08V (0.28 - 0.33C) (4330 Mod) |
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