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In regards to constructing the samples for the Embedment Test, does anyone know how or which way the aluminum is attached to the core? Is it possibly wrapped around the aluminum or is it stacked into the cells of the honeycomb core?

No, I was not on Boeing's portal just in the general supplier site. Thanks for the update.

We too are trying to resolve this same issue with Embedment Tests. I as well searched the Boeing supplier site to locate the document, D33080-1.926, Machine and Process Tools but have been unable to find it. Does someone have the link to assist me in locating that document? In addition to...