As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ERODED VERTICAL STAB LE PANEL 321E. REMOVED THE DAMAGE MATERIALS AND CLEAN. BONDED THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F SRM 55-30-01-2R-6 REFER TO SRM 51-70-07-0G-0 REV. 96.