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SAE AMS5223

Revision F, January 1, 2002

Complete Document

Iron-Nickel Alloy, Strip 49Fe - 5.3Cr - 42Ni - 2.5Ti - 0.55Al Solution Heat Treated, Cold Rolled, 10% Reduction

Includes all amendments and changes through Reaffirmation Notice , February 2012


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Product Details:

  • Revision: Revision F, January 1, 2002
  • Published Date: February 2012
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 6
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

Form:

This specification covers an iron-nickel alloy in the form of strip.

Application:

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 10-6 per degree Fahrenheit from -50 to +150 °F (-36 to +36 x 10-6 per degree Celsius from -46 to +66 °C) after suitable heat treatment, but usage is not limited to such applications.

AIA/NAS Aerospace Standards