As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STABILIZER PANEL MATING SURFACES ON THE RIGHT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAVE AREAS OF CHAFFING FROM CONTACT OF CLOSURE PANELS / [01] REMOVED FWD AND AFT RH SIDE SKATE ANGLES IAW SRM 51-40-02.;[02] INSTALLED RH FWD SKATE ANGLE IAW SRM 51-40-02.;[03] INSTALLED AFT R/H SKATE ANGLE PER SRM 51-40-02;[04] C/W INSPECTION;[05] C/W INSPECTION;[06] REMOVED AND REPLACED PER SRM 51-40-02