SAE AMS5661G
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Nickel-Iron Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 42.5Ni - 12.5Cr - 5.8Mo - 2.9Ti - 0.015B - 35Fe Consumable Electrode or Vacuum Induction Melted Solution, Stabilization, and Precipitation Heat Treated
Hardcopy , PDF
22-03-2024
English
17-08-2018
Important note : Users cannot be edited or removed once added to your Multi user PDF.1.1 Form This specification covers a corrosion and heat-resistant nickel-iron alloy in the form of bars, forgings, and flash-welded rings 5.0 inches (127 mm) and under in nominal diameter, or least distance between parallel sides, and stock of any size for forging or flash-welded rings (see 8.6). 1.2 Application These products have been used typically for parts, such as turbine discs, shafts, and blades, requiring higher strength than AMS5660 up to 1400 °F (760 °C) and oxidation resistance up to 1600 °F (871 °C), but usage is not limited to such applications.
| DocumentType |
Standard
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| Pages |
8
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
This specification covers a corrosion and heat-resistant nickel-iron alloy in the form of bars, forgings, and flash-welded rings 5.0 inches (127 mm) and under in nominal diameter, or least distance between parallel sides, and stock of any size for forging or flash-welded rings (see 8.6).
| SAE ARP1755B | Effect of Cleaning Agents on Aircraft Engine Materials Stock Loss Test Method |
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