AMS5707C: Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings and Rings 58Ni 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 - SAE International
Browse Standards AMS5707C
Historical REVISED 1970-05-01

Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings and Rings 58Ni 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 AMS5707C

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.

These products have been used typically for parts, such as cases, requiring high strength up to 1500 degrees F (816 degrees C) and oxidation resistance up 1750 degrees F (954 degrees C), but usage is not limited to such applications.

AMS5707N
2017-06-13
Latest
Revised
AMS5707M
2015-01-14
Historical
Revised
AMS5707L
2013-12-02
Historical
Reaffirmed
AMS5707K
2007-01-09
Historical
Revised
AMS5707J
2000-08-01
Historical
Revised
AMS5707H
1994-08-01
Historical
Revised
AMS5707G
1989-01-01
Historical
Revised
AMS5707F
1981-04-01
Historical
Revised
AMS5707E
1974-12-01
Historical
Revised
AMS5707D
1973-05-01
Historical
Revised
AMS5707C
1970-05-01
Historical
Revised
AMS5707B
1966-03-01
Historical
Revised
AMS5707A
1964-01-01
Historical
Revised
AMS5707
1963-07-01
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Purchase more aerospace standards and aerospace material specifications and save! AeroPaks offer a customized subscription plan that lets you pay for just the documents that you need, when you need them.

Get Involved

Want to participate in updating this standard?

X