Sheet and Plate, Magnesium Alloy, 2.0Th - 0.78Mn (HM21A - T8), Solution Heat Treated, Cold Worked, and Precipitation Heat Treated (Cancelled Jun 2006)
|
Product Code: AMS4390
Revision Number: K
Date Published: 2006-06-21
Issuing Committee:
Ams D Nonferrous Alloys Committee
Scope
This specification covers a magnesium alloy in the form of sheet and plate.
Product Status: In Stock
File Size:
97K
Purchase more aerospace standards and aerospace material specifications and save!
AeroPaks offers a customized subscription plan that lets you pay
for just the documents that you need, when you need them.
Learn more >
| Current & Historical versions of this standard |
| Standard |
Date published |
?Status |
| AMS4390K |
2006-06-21 |
Cancelled |
| AMS4390J |
1996-02-01 |
Noncurrent |
| AMS4390 |
1960-01-01 |
Issued |
|
Related Content
Papers
Books
Standards
- Magnesium Alloy, Sand Castings, 8.7Al - 0.70Zn - 0.26Mn (AZ91E-T6) Solution and Precipitation Heat Treated
- Aluminum Alloy, Plate, 5.0Cu - 0.4Mn – 0.5Mg - 0.4Ag (2139-T84), Solution Heat Treated, Cold Worked, and Artificially Aged
- Aluminum Alloy, Sheet and Plate, Alclad, 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024-O, Sheet and Plate) Annealed; or when specified, “As Fabricated” (2024-F)
|