As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER PREPARING THE REPAIR AREA ON THE VERTICAL STAB AUXILIARY PANEL DENT, FOUND A DISBONDED AREA OF APPROX 13" X 13" DUE TO CORROSION ON THE INNER SKIN. THIS DISBONDED AREA IS APPROX 14" FROM AUXILIARY SPAR & 56" FROM BOTTOM. REPAIRED LT VERTICAL STAB AUXILIARY PANEL INNER SKIN IAW SRM 51-70-10-2R REPAIR 4. MAJOR REPAIR.