by Rynoth » Wed Mar 11, 2015 2:27 pm
Hi Al, sorry you made that mistake but I think you'll find it's a relatively minor one now that you've sorted it out. A small amount of material actually needs to be removed at the root of the stab skins where it contacts the aft fuselage.
It will help us help you if you reference the plans page # (WIX-T08 or whatever) with your question, and if you post a new thread in this forum with the title of the plans page.
Page WIX-T09 says to "notch tip to clear ruddervator". It then calls to notch the fiberglass 7/8" (an approximation that worked for me.) On WIX-T10, that 3/4" reference is referring to the distance between the stabilator's tip rib (substructure) to the outside edge of the stabilator skin, which will be approximately the same as the distance between the inside edge of the fiberglass tip and the outside edge of the skin. Therefore, your notch would be 1/8" clear of the ruddervator (7/8" minus 3/4".) That said, my suggestion to you would be to wait to cut the fiberglass tip until you've completed the ruddervators and can pin them to the stabilators... then you'll know exactly how much fiberglass you need to trim. In a perfect world, the ruddervator ends on the exact same line as the outer edge of the stabilator skin, but that depends largely on the accuracy of placement of the piano hinges.
To forum admins, this discussion can probably be moved to a new topic under Waiexplans called "WIX-T08/T09 (Stabilator Skins/Tips)"
Edit - Split and renamed...