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Titanium Alloy Direct Deposited Products 6Al - 4V Annealed
- Aerospace Material Specification
Published September 26, 2016 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification covers metal products fabricated by direct metal deposition.
AMS4999A has been reaffirmed to comply with the SAE five-year review policy.
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|
Welcome to the SAE AMS AM, Additive Manufacturing public forum area.Scope: AMS AM is a technical committee in SAE’s Aerospace Materials Systems Group with the responsibility to develop and maintain aerospace material and process specifications and other SAE technical reports for additive manufacturing, including precursor material, additive processes, system requirements and post-build materials, pre-processing and post-processing, non-destructive testing and quality assurance.