SAE AMS4178C
Core, Flexible Honeycomb, Aluminum Alloy, Treated, for Sandwich Construction, 5052, 350 (177).
Standard:
AKA:
- AMS4178
- Revision: C
- 1995-11-01
- Historical. Access the latest revision: AMS4178E
- Ams D Nonferrous Alloys Committee
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 service up to 350 degrees F (177 degrees C) or for long-term service up to 200 degrees F (93 degrees C), but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4178E | 2008-10-21 | Latest | |
| AMS4178D | 2006-09-14 | Historical | |
| AMS4178C | 1995-11-01 | Historical | |
| AMS4178B | 1990-01-01 | Historical | |
| AMS4178A | 1983-01-01 | Historical | |
| AMS4178 | 1976-01-01 | Historical |
- SAE AMS 4178
- Aerospace
- Aluminum alloys
- Aluminum