UNLIMITED FREE ACCESS TO THE WORLD'S BEST IDEAS

close
Already an Engineering360 user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your Engineering360 Experience

close
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

SAE AMS4299

Aluminum Alloy, Plate (7449-T7951) 8.1Zn - 1.8Cu - 2.3Mg Solution Heat Treated, Stress Relieved, and Overaged

active, Most Current
Buy Now
Organization: SAE
Publication Date: 1 March 2018
Status: active
Page Count: 7
scope:

Form

This specification covers an aluminum alloy in the form of plate 0.50 to 2.50 inches (6.35 to 63.50 mm) inclusive, in nominal thickness (see 8.6).

Application

This product has been used typically for parts requiring high mechanical properties and moderate fracture toughness, but usage is not limited to such applications.

Document History

SAE AMS4299
March 1, 2018
Aluminum Alloy, Plate (7449-T7951) 8.1Zn - 1.8Cu - 2.3Mg Solution Heat Treated, Stress Relieved, and Overaged
Form This specification covers an aluminum alloy in the form of plate 0.50 to 2.50 inches (6.35 to 63.50 mm) inclusive, in nominal thickness (see 8.6). Application This product has been used...
January 1, 2005
Aluminum Alloy, Plate (7449-T7951) 8.1Zn - 1.8Cu - 2.3Mg Solution Heat Treated, Stress Relieved, and Overaged
Form: This specification covers an aluminum alloy in the form of plate. Application: This product has been used typically for parts requiring high mechanical properties and moderate fracture...
January 1, 2005
Aluminum Alloy, Plate (7449-T7951) 8.1Zn - 1.8Cu - 2.3Mg Solution Heat Treated, Stress Relieved, and Overaged
Form: This specification covers an aluminum alloy in the form of plate. Application: This product has been used typically for parts requiring high mechanical properties and moderate fracture...

References

Advertisement