The instructions tell me to use an angle drill to match drill the V/S rear spar using the 4 holes in the F-712E Tie Down Bar as a guide. In fact, there is no Tie Down Bar mounted on the inside of the very aft bulkhead of the fuselage (F-812A-1 and F-812C-1) and no hole in the bottom of the fuselage to screw in a tie down bolt if a bar were there. It's shown in the drawing, but nothing there. I talked with Van's and they are sending me stock to fabricate the Tie Down Bar but that leaves me with the problem of drilling out all the rivets holding the aft bulkhead in place so that I can attach it to the inside. I would have thought that this would have to have been installed in Manila during the construction of the fuselage.
Have any of you -8A QB guys had a similar experience?
Bill
Have any of you -8A QB guys had a similar experience?
Bill