I made the same mistake as noted here: https://vansairforce.net/threads/fi...8th-holes-in-hs-spar-web.208563/#post-1623421
I learned every word matters, and now know what "web" means.
So now I'm doing the rework, with the new VS web and new spar caps. It was a fairly cheap education ($330 for new spar caps, rear spar, and skin) and good practice, plus I have some realistic scraps I can practice on now too.
On the rework, I straightened the spar caps the best I could and am very happy with them, better than the first attempt. I flushed them up in the rear spar, drilled the web first this time. Then I went on to drill the flanges, and upon drilling the last hole into the first cap, I noticed there is hardly any meat left, nowhere near the minimum required; these will definitely crack. (They are 0.060" from edge of hole to edge of material, appx 0.100" from edge of material to centerline, and these are #40 rivets so just barely 1D from CL.)
Comparing to my old ones, sure enough, the replacement spar caps are noticeably shorter (but not enough that I caught it until I reached this point.)
Has anyone else encountered this? Should I go back to Van's and ask for replacement spar caps? Or, could I simply shorten the spar caps, removing that hole? I looked ahead in the plans and nothing jumps out at me indicating I couldn't shorten it to remove this hole. But, this is my first build so who knows what I'm missing there. I also figure it was originally designed to span the hole in question so I'm compromising a little bit of the designed strength by doing that.
Attached are some images that show:
I learned every word matters, and now know what "web" means.
So now I'm doing the rework, with the new VS web and new spar caps. It was a fairly cheap education ($330 for new spar caps, rear spar, and skin) and good practice, plus I have some realistic scraps I can practice on now too.
On the rework, I straightened the spar caps the best I could and am very happy with them, better than the first attempt. I flushed them up in the rear spar, drilled the web first this time. Then I went on to drill the flanges, and upon drilling the last hole into the first cap, I noticed there is hardly any meat left, nowhere near the minimum required; these will definitely crack. (They are 0.060" from edge of hole to edge of material, appx 0.100" from edge of material to centerline, and these are #40 rivets so just barely 1D from CL.)
Comparing to my old ones, sure enough, the replacement spar caps are noticeably shorter (but not enough that I caught it until I reached this point.)
Has anyone else encountered this? Should I go back to Van's and ask for replacement spar caps? Or, could I simply shorten the spar caps, removing that hole? I looked ahead in the plans and nothing jumps out at me indicating I couldn't shorten it to remove this hole. But, this is my first build so who knows what I'm missing there. I also figure it was originally designed to span the hole in question so I'm compromising a little bit of the designed strength by doing that.
Attached are some images that show:
- the spar cap is flush with the bottom of the rear spar
- the final hole is extremely close to the edge
- and with the reworked spar cap cleco'd in (in the back), the original spar cap is butted up in the front to show the length difference and the remaining metal