Titanium Alloy Direct Deposited Products 6Al - 4V Annealed
- Aerospace Material Specification
Published September 26, 2016 by SAE International in United States
This specification covers metal products fabricated by direct metal deposition.
AMS4999A has been reaffirmed to comply with the SAE five-year review policy.
|Aerospace Material Specification||Aluminum Alloy, Die Forgings 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7452) Solution Heat Treated, Compression Stress-Relieved, and Overaged|
|Aerospace Material Specification||Aluminum Alloy Forgings and Rolled Rings 4.4Cu - 0.85Si - 0.80Mn - 0.50Mg (2014-T6) Solution and Precipitation Heat Treated|
|Aerospace Material Specification||Aluminum Alloy, Hand Forgings 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7452) Solution Heat Treated, Compression Stress-Relieved, and Overaged|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|TABLE 3||RADIOGRAPHIC INSPECTION ACCEPTANCE CRITERIA|
|TABLE 4A||PROCESS APPROVAL TENSILE PROPERTIES, INCH/POUND UNITS|
|TABLE 4B||PROCESS APPROVAL TENSILE PROPERTIES, SI UNITS|
|TABLE 5A||PRODUCTION HARDWARE APPROVAL TENSILE PROPERTIES, INCH/POUND UNITS|
|TABLE 5B||PRODUCTION HARDWARE APPROVAL TENSILE PROPERTIES, SI UNITS|
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