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There were 2 carbon locating dowels for each panel; here I have already roughed them up with 80 grit sandpaper prior to test fitting. I tested each dowel to ensure it reached to the next rib prior to gluing in place.
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The locating dowels/antirotation pins installed in the wing.
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Tail cutout -- I also ironed down a small edge here to keep the covering from peeling back.
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After marking the stab's position on the fuselage, I "cut" the covering with soldering iron. This way there's no chance of an Xacto cutting into the wood and weakening the stab. (The stab's fit into the fuse was very tight -- great!)
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