SAE AMS4095B
Aluminum Alloy, Sheet and Plate, Alclad 6.3cu 0.30mn 0.18zr 0.10v 0.06ti, Alclad 2219 T31; Sheet, Solution Heat Treated and Cold Worked Alclad 2219-T351; Plate, Solution Heat Treated and Stress Relieved.
Standard:
AKA:
- AMS4095
- Revision: B
- 2000-09-01
- 1993-10-01
- Historical. Access the latest revision: AMS4095C
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet and plate.
These products have been used typically for parts requiring high strength up to 600 degrees F (316 degrees C) and are well suited for cryogenic applications and where welding and maximum corrosion resistance are required, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment; ARP823 recommends practices to minimize such conditions.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4095C | 2004-11-17 | Latest | |
| AMS4095B | 1993-10-01 | Historical | |
| AMS4095A | 1992-04-01 | Historical | |
| AMS4095 | 1969-11-01 | Historical |
- SAE AMS 4095
- Aerospace
- Aluminum alloys
- Aluminum