Core, Flexible Honeycomb, Aluminum Alloy, Treated for Sandwich Construction, 5052, 350 (177).
|
Product Code: AMS4178
Revision Number: E
Date Published: 2008-10-21
Issuing Committee:
Ams D Nonferrous Alloys Committee
Scope
This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form. This honeycomb core has been used typically in contoured sandwich construction for short-term exposure up to 350 °F (177 °C) or for long-term exposure up to 200 °F (93 °C), but usage is not limited to such applications.
Product Status: In Stock
File Size:
1536K
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 |
| AMS4178E |
2008-10-21 |
Revised |
| AMS4178D |
2006-09-14 |
Revised |
| AMS4178C |
1995-11-01 |
Revised |
| AMS4178B |
1990-01-01 |
Revised |
| AMS4178A |
1983-01-01 |
Revised |
| AMS4178 |
1976-01-01 |
Issued |
|
Related Content
|