As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LH UPPER WING TO FUSELAGE SUPPORT ANGLE. JUST FWD OF FRAME 41 HAS EVIDENCE OF 1/4" CRACK. PROCEEDING DOWNWARD FROM THE RIVET. -C/A-REPAIRED LH UPPER WING TO FUSELAGE SUPPORT ANGLE JUST FWD OF FRAME 41 IAW SRM 53-23-12. SEE NRTC E683553 FOR PAINT.