Titanium Alloy Sheet, Strip, and Plate 6al 6v 2sn Solution Heat Treated and Aged
|
Product Code: AMS4990
Date Published: 2003-04-17 - A newer version of this standard is available.
Issuing Committee:
Ams G Titanium And Refractory Metals Committee
Scope
This specification covers a titanium alloy in the form of sheet, strip, and plate. This material is typically used for parts requiring high strength-to- weight ratio and stability up to 550 degrees F (288 degrees C), but usage is not limited to such applications. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.
Product Status: In Stock
File Size:
77K
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 |
| AMS4990A |
2009-09-02 |
Revised |
| AMS4990 |
2003-04-17 |
Issued |
|
Related Content
|