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SAE AMS5598 Revision E, July 1, 2007
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Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95 (Cb (Nb) + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode, Remelted or Vacuum Induction Melted, Solution Heat Treated, Precipitation-Hardenable
Includes all amendments and changes through Reaffirmation Notice , October 2012
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AIA/NAS Aerospace Standards

This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate procured in inch/pound units.


These products have been used typically for parts requiring high strength up to 1500 ºF (816 ºC) and oxidation resistance up to 1800 ºF (982 ºC) and for bellows and flat springs requiring optimum resistance to relaxation up to 1000 ºF (538 ºC) with moderate or relatively low stresses, particularly where welding is involved, but usage is not limited to such applications. Parts may be formed, welded if required, and then heat treated to improve strength at elevated temperatures.