As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT VERTICAL STAB CLOSURE ANGLE ON TOP OF FUSELAGE AFT OF STA 1016 HAS CHAFFING DAMAGE / CHAFFING ON THE LH VERTICAL STAB CLOSURE ANGLE ON TOP OF FUSELAGE AFT OF STA 1016 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM NEED TO REMOVE AND REPLACE IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED LH VERTICAL STAB CLOSURE ANGLE IAW SRM 51-40-02 AND IAW DWG# 143A8300