Shaved the aft fuselage floor spacers, F21-10, down to 0.093 from 0.125 to compensate for the 0.032 thickness of the lower cross tie, F19-05.
Ground off some of the elevator horn flange where it contacted the upper center vert stabilizer bolt. Used POR15 to touchup the powder coat. When I had clearance with the horn, I needed to trim more of the rudder skin to achive contact of the elevator horn stop with the rubber post.
Started working on rudder cable clearance where it exits the skin.
Updrilled, deburred, primed and riveted the hor. stab. fwd attach bracket, T04-06.
Smoothed hor.stab fwd skin that was trimmed to fit around the aft side skins.
