Stuart Grant
Active Member
I am finalizing flight control hookup and installed the wings for the first time so I could match drill the flaperon torque tubes. No seals are installed on the sides of the fuselage yet. The left wing went in all the way but the right wing was about 1/2" shy of the spar holes lining up. I was able to get things in far enough to do the match drilling successfully and pulled things apart and put the wings back in the rack.
The friend that was helping by carrying the spar end of the wing suggested that I file the sharp edges of the main spar a bit because the were tough on his skin and I said "no, no you cant do that." I do see that the instructions say "if the stub spar interferes with installation of the wing the stub spar may require local dressing with a file." After moving the fuselage back into my garage I noticed some big scratches on the bottom of the slot where the main spars had slid in. There were also scratches on the faces of one the spars. Maybe this is a question for Van's Tech Support but I am wondering if it is OK to ease the sharp edges of the main spar ends with a file to reduce scratching? I plan to install and remove the wings many, many times.
The friend that was helping by carrying the spar end of the wing suggested that I file the sharp edges of the main spar a bit because the were tough on his skin and I said "no, no you cant do that." I do see that the instructions say "if the stub spar interferes with installation of the wing the stub spar may require local dressing with a file." After moving the fuselage back into my garage I noticed some big scratches on the bottom of the slot where the main spars had slid in. There were also scratches on the faces of one the spars. Maybe this is a question for Van's Tech Support but I am wondering if it is OK to ease the sharp edges of the main spar ends with a file to reduce scratching? I plan to install and remove the wings many, many times.