the reason it seems off from what you've seen done with it is because the companies who tend to make use of it already know its strengths, weaknesses and tolerances enough to know that even if it worked, and worked well, it wouldn't work for long. and i dont want to make up excuses as to why it wouldn't work, i'm just saying it wouldn't because realistically it just wouldn't. Airframes aren't subjected to the same sheer forces tools would be, significant forces sure, but not the same, and the reason they would use it is because of its relative strength/weight ratio, but what you're suggesting has nothing to do with aircraft, and there's alot of good reasons people dont use titanium to make tools, cost being a technically irrelevant one to this conversation, but its lack of viscosity being one of the major ones.
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