As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CHAFING FOUND ON FUSELAGE SKINS, BETWEEN 2108 & 2184 AT STRINGER 1 - 3R AT VERT FIN. INTERIM REPAIR DOUBLER INSTALLED IAW ECRA 5330-05503 REV 0 PART 1 3. DIP IS REQUIRED TO ACCOMPLISH INSPECTIONS IAW PART 2 OF ECRA, PRIOR TO 30000 CYCLES, PLANNING OR TOMC TO CONTACT EG AFTER 28000 BUT BEFORE 29000 CYCLES.