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SAE AMS5704E

Nickel Alloy, Corrosion and Heat Resistant, Forgings 57Ni 19.5Cr 13.5Co 4.3Mo 3.0Ti 1.4Al 0.05Zr 0.006B, Consumable Electrode or Vacuum Induction Melted, 1825 to 1900°F (996 to 1038°C) Solution, Stabilization, and Precipitation Heat Treated.

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Standard:
  • AMS5704
  • Revision: E
Revised:
  • 1993-10-01
Revision:
  • Historical. Access the latest revision: AMS5704J
Issuing:
  • Ams F Corrosion Heat Resistant Alloys Committee
Scope:

This specification covers a corrosion and heat resistant nickel alloy in the form of forgings and forging stock.

These forgings have been used typically for rotating parts, such as compressor blades, discs, hubs, shafts, and spacers requiring high strength up to 1500 degrees F (816 degrees C) and oxidation resistance up to 1750 degrees F (954 degrees C), but usage is not limited to such applications.

History:
StandardPublishedRevisionStatus
AMS5704J2008-03-27LatestRevised
AMS5704H2006-05-17HistoricalRevised
AMS5704G2000-10-01HistoricalRevised
AMS5704F1995-04-01HistoricalRevised
AMS5704E1993-10-01HistoricalRevised
AMS5704D1988-04-01HistoricalRevised
AMS5704C1982-01-01HistoricalRevised
AMS5704B1976-01-01HistoricalRevised
AMS5704A1970-05-01HistoricalRevised
AMS57041966-03-01HistoricalIssued
AKA:
  • SAE AMS 5704
Sector:
  • Aerospace
Topic:
  • Metallurgy
  • Metals
  • Nickel
  • Materials properties

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