Brief Description: Cross Brace Tabs Added to Right Outer Wing Support
Center punched all of the tabs available. Drilled each one with a 3/16 inch hole on each end. Ground off each hole to remove the burrs. Placed each tab in the vice and bent it out at about a 30 deg angle. Also drilled the double tab with a hole at each end and one in the center.
Drilled a 3/16 inch hole in each end of the wing support between the second and forth rivet holding the flanges on. Placed an AN3-21A bolt through each hole and added one tab and secured it with a self locking nut. Repeated the process on the second wing support.
