Aluminum Alloy, Alclad Sheet and Plate 4.3cu 1.4mg 0.60mn (Alclad 2524-T3) Solution Heat Treated and Cold Worked

Standard:
Revised:
  • 2003-08-31
 
  • HISTORICAL Access the latest revision: AMS4296C
Publisher:
  • SAE International
Pages:
7
Scope:

This speicification covers an aluminum alloy in the form of sheet and plate clad on both sides.

These products have been used typically for formed structural aircraft parts requiring improved resistance to fatigue crack growth and high toughness with strength similar to Alclad 2024-T3, but usage is not limited to such applications.

Certain design and processing procedures may cause these products to be come susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

History:
Standard Published Revision Status
AMS4296C 2017-10-13 Latest Revised
2012-02-15 Historical Reaffirmed
2003-08-31 Historical Revised
1997-09-01 Historical Issued
AKA:
  • SAE AMS 4296
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