SAE AMS5225E
Iron-Nickel Alloy, Strip, 49Fe - 5.3Cr - 42Ni - 2.5Ti - 0.55Al, Solution Heat Treated, Cold Rolled, 50% Reduction.
Standard:
AKA:
- AMS5225
- Revision: E
- 2006-04-18
- 2000-05-04
- Historical. Access the latest revision: AMS5225F
- Ams F Corrosion Heat Resistant Alloys Committee
This specification covers an iron-nickel alloy in the form of strip.
This strip has been used typically for diaphragms, leaf springs, and helical springs, requiring a precipitation-hardenable alloy with a coefficient of modulus of elasticity of -20 to +20 x 10e-6 per degree Fahrenheit from -50 to +150F (-36 to +36 x 10e-6 per degree Celsius from -46 to +66C) after suitable heat treatment.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5225F | 2009-04-14 | Latest | |
| AMS5225E | 2000-05-04 | Historical | |
| AMS5225D | 1994-04-01 | Historical | |
| AMS5225C | 1982-04-01 | Historical | |
| AMS5225B | 1974-12-01 | Historical | |
| AMS5225A | 1963-07-01 | Historical | |
| AMS5225 | 1955-08-01 | Historical |
- SAE AMS 5225
- Aerospace
- Metallurgy
- Metals
- Nonferrous alloys
- Materials properties