I am working on the floor aft of bulkhead A. I was considering using thicker
material from A to B, And the same forward of A when I get to that point. I
was thinking .025 or .032. I don't want to add unnecessary weight, but the
.020 seems like it would dent very easily when you are crawling around on
your knees back there.
Does this seem to be an issue with heavily used airplanes?
Thanks
Jesse
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