SAE AMS4147E-2018 PDF

Scope: Form This specification covers an aluminum alloy in the form of die forgings up to 4 inches@ incl (102 mm@ incl) in thickness@ and hand forgings up to 6 inches@ incl (152 mm@ incl) in thickness (see 8.6). Application These forgings have been used typically for parts requiring a combination of good strength and resistance to stresscorrosion cracking@ and where good stability is required during machining@ but usage is not limited to such applications.

SAE AMS4147E-2018 history

2018 SAE AMS4147E-2018 Aluminum Alloy Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7352) Solution Heat Treated@ Stress Relieved by Compression@ and Overaged (UNS A97075)
2012 SAE AMS4147D-2012 Aluminum Alloy Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7352) Solution Heat Treated, Stress Relieved by Compression, and Overaged
2011 SAE AMS4147B-2011 ALUMINUM ALLOY FORGINGS 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr(7075-T7352) Solution Heat Treated, Stress Relieved by Compression, and Overaged
2007 SAE AMS4147D-2007 Aluminum Alloy Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7352) Solution Heat Treated@ Stress Relieved by Compression@ and Overaged (UNS A97075)
2000 SAE AMS4147C-2000 Aluminum Alloy Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr(7075-T7352) Solution Heat Treated, Stress Relieved by Compression, and Overaged
1992 SAE AMS4147C-1992 Aluminum Alloy, Forgings 5.6Zn 2.5Mg 1.6Cu 0.23Cr Solution Heat Treated, Stress Relieved by Compression, and Overaged
1978 SAE AMS4147A-1978 ALUMINUM ALLOY FORGINGS 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7352)
1968 SAE AMS4147-1968 ALUMINUM ALLOY FORGINGS 5.6Zn - 2.5Mg - 1.6Cu - 0.30Cr (7075-T7352) Stress Relief Compressed