As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STAB CORRODED ON THE LT & RT PLATES REAR SPAR BETWEEN HSS 150-160. THE CORROSION WAS REMOVED. UT INSPECTION WAS ACCOMPLISHED IAW SPM 04-00-07 PAR. 5 FIG. 3 SHEET 1 AND 2. FOUND TO BE WITHIN LIMITS IAW SRM 55-02 PAR. 24 FIG. 28.