The slotted flap hinges will have the metal washers replaced with smaller 1" nylon type.
Below the tie down is formed in the corner against spar and one rib. I layed in a thin flox layer in the bottom to create a flat bed along the bottom, then layed down the bid as per the manual with the bottom layer being 16 bid thick. I then bonded in a 1/4" 2x2 block of phenolic with a 1/4" nit plate riveted in place. A VOR antenna is installed in the right wing and a Glide Slope antenna in the left.
Below is the drive rib installed for the aileron. It has the metal fork installed which is hanging out the bottom skin 1". The three bolts on the fork bracket have metal locknuts on them and a dab of S-adhesive as well for protection. They are not accessible in the future.
Below are the two u-shaped carbon fiber pieces I fabricated which are the bolt bracket, for the aileron bell crank pivot points. The first photo shows them in the fabrication blocks and then they are in place in the wing. Temporary foam support walls are shown in place, supporting the 4 bid carbon fiber walls which anchor down the bell crank pivot point to surrounding surfaces. The drive tube connecting to the aileron can also bee seen in the photo.
Below are the lead balance weights for the tips of the ailerons.
Both root bays have Inspection/Adj. access panels installed on lower skin as per Canadian Inspector request to meet annual inspection/adj. requirements.
Following are construction of the flanges to go inside wing upper edge for supporting top skins and a picture of the left tip bay with chrome pitot bracket installed.
Wing walk support braces are installed and the top wing skin panels are going on.
Wing top panels were all long board sanded down and layers of glass cloth added to the top of the left and right wings of this one piece EX wing. Slotted flap units are installed and awaiting the glass covering over their leading edges.
