As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT UPPER WING SKIN CORRODED AT MID SPAR C-T FUSELAGE. [SUP 06-06-07] PERFORMED DETAILED VISUAL INSPECTION OF THE LT FWD TRUNNION FUSE PINS FOR LOOSE FUSE PINS AND CORROSION ON ADJACENT STRUCTURE. WORK ACCOMPLISHED PER UA ENGINEERING EVALUATION AND RECOMMENDED REPAIR.