SAE AMS6522C PDF
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Steel Plate 2.0Cr – 10Ni – 14Co – 1.0Mo (0.13 – 0.17C) Vacuum Melted, Normalized, and Overaged(NONCURRENT Apr 2005)
Description
This specification covers a premium aircraft-quality alloy steel in the form of plate.
History
| AMS6522D | 2016-02-17 | Latest | Stabilized |
| AMS6522C | 2011-05-26 | Historical | Reaffirmed |
| AMS6522B | 2003-07-14 | Historical | Revised |
| AMS6522A | 1994-04-01 | Historical | Reaffirmed |
| AMS6522 | 1981-04-01 | Historical | Issued |
| ISSUING COMMITTEE | AMS E Carbon and Low Alloy Steels Committee |
|---|---|
| DATE | 2011-05-26 |
| DOI | |
| ISCURRENT | |
| PAGE | 7 |
| PUBLISHER | SAE International |
| REVISED | REAF. NONC. |
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