sdar79
Aerospace
- Feb 8, 2012
- 15
Is there any published data to go by for PH13-8MO in the solution treated/annealed condition? MMPDS and the other references we have in our office say that 13-8 should not be used in this condition but do not say why. We have some CSI's on our aircraft that should be heat treated to the H1000 condition, but some suppliers have been ignoring this requirement and shipping parts in the solution treated condition instead.