SAE AMS6522D
Current
The latest, up-to-date edition.
Steel Plate 2.0Cr - 10Ni - 14Co - 1.0Mo (0.13 - 0.17C) Vacuum Melted, Normalized, and Overaged
Hardcopy , PDF
English
17-02-2016
1 SCOPE
2 APPLICABLE DOCUMENTS
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 ACKNOWLEDGMENT
7 REJECTIONS
8 NOTES
Specifies a premium aircraft-quality alloy steel in the form of plate.
| DocumentType |
Standard
|
| Pages |
7
|
| ProductNote |
THIS VERSION IS NOW STABILIZED
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
This specification covers a premium aircraft-quality alloy steel in the form of plate.
| SAE AMS2248H | Chemical Check Analysis Limits, Corrosion- and Heat-Resistant Steels and Alloys, Maraging and Other Highly Alloyed Steels, and Iron Alloys |
| SAE AMS2370L | Quality Assurance Sampling and Testing Carbon and Low-Alloy Steel Wrought Products and Forging Stock |
| SAE AMS2750E | Pyrometry |
| ASTM E 8M : 2004 | Standard Test Methods for Tension Testing of Metallic Materials [Metric] (Withdrawn 2008) |
| ASTM E 353 : 2014 : REDLINE | Standard Test Methods for Chemical Analysis of Stainless, Heat-Resisting, Maraging, and Other Similar Chromium-Nickel-Iron Alloys |
| SAE AMS2300L | Steel Cleanliness, Premium Aircraft-Quality Magnetic Particle Inspection Procedure |
| ASTM E 8 : 2004 | Standard Test Methods for Tension Testing of Metallic Materials |
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