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SAE AMS4298

Aluminum Alloy, Alclad Sheet 3.8Cu - 1.0Mg - 0.30Mn - 0.60Zn (Alclad 2056-T3) Solution Heat Treated and Cold Worked

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Organization: SAE
Publication Date: 1 April 2016
Status: active
Page Count: 6
scope:

Form:

This specification covers an aluminum alloy in the form of sheet 0.063 to 0.236 inch (1.60 to 6.00 mm), incl, in thickness, clad on both sides (see 8.4).

Application:

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 become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

 

 

 

 

Document History

SAE AMS4298
April 1, 2016
Aluminum Alloy, Alclad Sheet 3.8Cu - 1.0Mg - 0.30Mn - 0.60Zn (Alclad 2056-T3) Solution Heat Treated and Cold Worked
Form: This specification covers an aluminum alloy in the form of sheet 0.063 to 0.236 inch (1.60 to 6.00 mm), incl, in thickness, clad on both sides (see 8.4). Application: These products have...
July 1, 2004
Aluminum Alloy, Alclad Sheet 3.8Cu - 1.0Mg - 0.30Mn - 0.60Zn (Alclad 2056-T3) Solution Heat Treated and Cold Worked
Form: This specification covers an aluminum alloy in the form of sheet clad on both sides. Application: These products have been used typically for formed structural aircraft parts requiring improved...
July 1, 2004
Aluminum Alloy, Alclad Sheet 3.8Cu - 1.0Mg - 0.30Mn - 0.60Zn (Alclad 2056-T3) Solution Heat Treated and Cold Worked
Form: This specification covers an aluminum alloy in the form of sheet clad on both sides. Application: These products have been used typically for formed structural aircraft parts requiring improved...

References

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