SAE AMS4221E
Current
The latest, up-to-date edition.
ALUMINUM ALLOY, PLATE, 4.4CU - 1.5MG - 0.60MN (2124-T8151) SOLUTION HEAT TREATED, STRESS RELIEVED, AND PRECIPITATION HEAT TREATED
Hardcopy , PDF
English
13-12-2016
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1 SCOPE
2 APPLICABLE DOCUMENTS
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 ACKNOWLEDGMENT
7 REJECTIONS
8 NOTES
This specification covers an aluminum alloy in the form of plate 1.500 inches (38.10 mm) to 6.000 inches (152.40 mm) in nominal thickness (see 8.4).
| Committee |
AMS-D
|
| DocumentType |
Revision
|
| Pages |
7
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| ANSI H35.2 : 2017 | DIMENSIONAL TOLERANCES FOR ALUMINUM MILL PRODUCTS |
| ASTM B 666/B666M : 2015 : REDLINE | Standard Practice for Identification Marking of Aluminum and Magnesium Products |
| SAE ARP 1917 : 2002 | CLARIFICATION OF TERMS USED IN AEROSPACE METALS SPECIFICATIONS |
| SAE AMS 2772 : 2016 | HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS |
| SAE AMS2355L | QUALITY ASSURANCE, SAMPLING AND TESTING, ALUMINUM ALLOYS AND MAGNESIUM ALLOY, WROUGHT PRODUCTS (EXCEPT FORGING STOCK), AND ROLLED, FORGED, OR FLASH WELDED RINGS |
| ASTM B 660 : 2015 : REDLINE | Standard Practices for Packaging/Packing of Aluminum and Magnesium Products |
| ANSI H35.2M : 2013 | DIMENSIONAL TOLERANCES FOR ALUMINUM MILL PRODUCTS (METRIC) |
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