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Full Description

This specification has been declared "NONCURRENT" by the Aerospace Materials Diviaion, SAE, as of September 2001. It is recommended, therefore, that this specification not be specified for new designs.

“NONCURRENT” refers to those materials which have previously been widely used and which may be required on some existing deigns in the future. The Aerospace Materials Division, however, does not recommend these as standard materials for future use in new designs.
 

Document History

  1. SAE AMS5669B


    Alloy Bars, Corrosion and Heat Resistant Nickel Base - 15.5Cr - 0.95 (Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted (Stabilized: May 2014)

    • Most Recent
  2. SAE AMS5669A

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    Alloy Bars, Corrosion and Heat Resistant, Nickel Base - 15.5Cr - 0.95 (Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe, Consumable Electrode or Vacuum Induction Melted

    • Historical Version