We have a 7075 Al pump housing that has currently undergone a T651 temper but requires a T751 treatment to alleviate stress corrosion cracking.
Is it necessary to re-stretch a 7075 aluminum part to relieve internal stresses after a T751 heat treatment (Solution heat treated and stretched to remove internal stresses then overaged/stabilized) when a T651 (Solution heat treated and stretched to remove internal stresses then artificially aged) heat treatment was performed just previously?
The part will only be held at minimum over-age temperatures to alleviate SCC in order to maintain most of the tensile and yield strength of the material.