While performing step 7 on page 21-13 of the instructions, I was hand twisting a #12 drill bit remove the powder coating from inside the holes on the WD-1210-PC. One of the pairs of tabs has two holes and fortunately, I chose to push the drill bit straight through to remove the powder coating from the opposite hole. I quickly realized there was a hole alignment issue. Had I dressed each hole from the outside, the alignment issue may not have been noticed until way after the WD-1210-PC control column was sealed in place by the fuselage?s corner skins.
I would highly suggest fellow builders working on the fuselage check their WD-1210-PC control column to ensure all your holes are in good alignment. Sent an Email to Van?s support about this with a photo on Friday, but have not received a reply as of yet.
A friend pointed out one of the tabs is longer than the other. Guessing the tabs must be predrilled prior to welding. One being longer would explain the misalignment.
I would highly suggest fellow builders working on the fuselage check their WD-1210-PC control column to ensure all your holes are in good alignment. Sent an Email to Van?s support about this with a photo on Friday, but have not received a reply as of yet.
A friend pointed out one of the tabs is longer than the other. Guessing the tabs must be predrilled prior to welding. One being longer would explain the misalignment.