As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING LEADING EDGE PANEL NR 612 DB HAS LANDING AREA INTERIOR LAMINATE WORN/TORN. REPAIRED THE DAMAGED AREA BY APPLYING ALUMINUM FOIL IAW SRM 57-41-12. REMOVED & REATTACHED THE PANEL RESTRAINING CORDS REF AMM 57-41-41-4. PREPPED THE BONDING SURFACE FOR THE FOIL APPLICATION REF SRM 57-41-12. ALODINED THE SURFACE REF SRM 51-21-10. PRIMED THE SURFACE REF SRM 51-23-10.