While assembling my center section I was surprised to find a burr on an anodized part F-804G-1.From what I can tell of the rest of these parts they seem to all have a very good job of minimal material removed deburring prior to being anodized. Prior to that I found several tipped rivets (enough to be questioned) on the center section assembly that is completed by Vans. My wing had a rivet on the spar that was wayyyy over driven in width and height. Build support said drill it out and replace with AN3 bolt since I have no way to squeeze a -6 rivet
Now I’m wondering what burrs lie under what is pre-assembled on the spar and center section.
I deburred and primed and moved on but just wondering what’s up with QA/QC on such major parts.
Now I’m wondering what burrs lie under what is pre-assembled on the spar and center section.
I deburred and primed and moved on but just wondering what’s up with QA/QC on such major parts.