Thanks for all the suggestions.
The piece to the side of the hole (which has been drilled out in the second picture) is to placed behind the skin as a doubler. Will be riveted to the skin from within the wing. I have access from the wing tip. I did make a circular version (per AC43-13) however found the rectangular version easier to conform to the leading edge. The question becomes, what is the best filler to place in the defect once the doubler is placed behind the skin. I have fashioned a circular piece but fixing(riveting) would warp the piece given the small seize.Thought there might be an established filler approach. AC43 does not discuss this.
To answer some questions, the pictures may not be that clear but AC circular doubler is 2.5 " in diameter suggesting 8 rivets angled a t 45 degrees. There are 8 on this doubler which is not larger the 2.5 " and the rivet/drill distances are within "code" of 4-6D. Already have a pitot/AOA Garmin mounted to wing. Already have the Premier Z-tip landing lights ready for installation. JD weld sounds like a good idea. Would consider new skin as the very last resort.
Would any consider patching with West System Epoxy Resin and sanding this down to conform with the remaining wing?
Hoping Vans has something soon and will share with the group when I hear of something.
Thanks again.