When I fabricated the control column bearing brackets in which the control column pivots, the bearings would not turn freely. I guess when I squeezed all those an470-4's around the bearing, the bearing got stressed some way. I put an AN3 bolt in it and could swivel it around but it was stiff. I (mistakenly, I think now) decided to go ahead and rivet the brackets onto the bulkhead, which has now been installed onto the seat ribs, thinking that it is the bolt that will be turning inside the bearing. But now I realize that the bolt will be jammed up tight against the bearing and it will be the bearing itself that will be turning - not the bolt inside the bearing. (I hope this isn't too confusing). Now my question: Is it VERY important that there is no binding in these bearings? If it is, then I should try to drill out all 16 LP4-3 rivets in each bracket where they are riveted to the seat-front bulkhead (if I can still reach them) and refabricate those bearing brackets.
I don't want to find out on the first flight that my stabilator control has a "stiff" spot. Has anyone else encountered this and are there any any suggestions???
I don't want to find out on the first flight that my stabilator control has a "stiff" spot. Has anyone else encountered this and are there any any suggestions???