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SAE AMS5703

Revision D, September 2006

Complete Document

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 41.5Ni - 16Cr - 37Fe - 2.9Cb - 1.8Ti Consumable Electrode or Vacuum Induction Melted 1750 °F (954 °C) Solution, Stabilization, and Precipitation Heat Treated

Includes all amendments and changes through Reaffirmation Notice , February 2012


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Product Details:

  • Revision: Revision D, September 2006
  • Published Date: February 2012
  • Status: Historical
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 7
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

Form

This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.

Application

These products have been used primarily for parts requiring a combination of resistance to creep and stress-rupture up to 1300 °F (704 °C), oxidation resistance up to 1800 °F (982 °C), and good machinability, but usage is not limited to such applications.
AIA/NAS Aerospace Standards