Guys and Gals,
We picked up our QB wings last summer, but left them crated until recently. I removed the first (left) wing from the crate in January and we put it on the bench to inspect it. Of course it was oily from the WD-40 sprayed on in the Phillipines, and as I wiped the top surface down, I noticed general conformity to the NACA2013.5 airfoil everywhere except at the root. Here, there was a deformity. Laying a straight edge from the spar area, forward along the wing/tank root rivet line, there is a concavity where the ruler bridges three rivets before touching down on the convex curve to the leading edge.
This was upsetting! I thought there must be some easy explanation like the "Z" brackets not being tightened, etc, but we checked them and they were all tight (actually overtightened). We removed the tank and inspected the top skin which seemed to be slightly divergent on the trailing edge at the root. Also, it seemed that the Proseal had been layed in behind the aft tank skin seam to possibly cause interference with the spar when in place. BTW, the bottom skin exhibits a coresponding bulge (convexity) in sympathy with the top skin.
A call to Van's builder support was a bit surprising in that the initial listener's response seemed to be mildly incredulous that I was concerned?!?!? When I explained that I preferred my top wing skins to exhibit a convex conformity to the airfoil profile it was suggested that I remove the tank and open up the holes in the spar where the "Z" brackets are bolted to change the tanks vertical orientation on the spar for the fix. This was done, but the skin still exhibits some slight concavity in this root area. The tip end of the tank is perfect and the "Z" bracket holes in the spar were not changed here.
I have since removed the tank again and attempted to cautiously press on the skin overhang behind the aft tank seam to put some small convex shape in the overhanging skin. It would almost seem as there may be interference with the top skin/tank seam and the spar, that is pushing the tank out of position. Presently, the tank is still sitting on the workbench and I thought perhaps a note to the Forum would be in order before re-installing.
Would anyone have any comments or suggestions on this anomoly?
Thanks, Pete
(pic posted down a few posts)
We picked up our QB wings last summer, but left them crated until recently. I removed the first (left) wing from the crate in January and we put it on the bench to inspect it. Of course it was oily from the WD-40 sprayed on in the Phillipines, and as I wiped the top surface down, I noticed general conformity to the NACA2013.5 airfoil everywhere except at the root. Here, there was a deformity. Laying a straight edge from the spar area, forward along the wing/tank root rivet line, there is a concavity where the ruler bridges three rivets before touching down on the convex curve to the leading edge.
This was upsetting! I thought there must be some easy explanation like the "Z" brackets not being tightened, etc, but we checked them and they were all tight (actually overtightened). We removed the tank and inspected the top skin which seemed to be slightly divergent on the trailing edge at the root. Also, it seemed that the Proseal had been layed in behind the aft tank skin seam to possibly cause interference with the spar when in place. BTW, the bottom skin exhibits a coresponding bulge (convexity) in sympathy with the top skin.
A call to Van's builder support was a bit surprising in that the initial listener's response seemed to be mildly incredulous that I was concerned?!?!? When I explained that I preferred my top wing skins to exhibit a convex conformity to the airfoil profile it was suggested that I remove the tank and open up the holes in the spar where the "Z" brackets are bolted to change the tanks vertical orientation on the spar for the fix. This was done, but the skin still exhibits some slight concavity in this root area. The tip end of the tank is perfect and the "Z" bracket holes in the spar were not changed here.
I have since removed the tank again and attempted to cautiously press on the skin overhang behind the aft tank seam to put some small convex shape in the overhanging skin. It would almost seem as there may be interference with the top skin/tank seam and the spar, that is pushing the tank out of position. Presently, the tank is still sitting on the workbench and I thought perhaps a note to the Forum would be in order before re-installing.
Would anyone have any comments or suggestions on this anomoly?
Thanks, Pete
(pic posted down a few posts)
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