As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT SIDE FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE BS 1016 - BS 1132 HAS CHAFFING DAMAGE / EVALUATED CHAFFING DAMAGE ON L/H CLOSURE ANGLE BS 1016 - BS 1132. FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED NEW LH CLOSURE ANGLE FROM BS 1016 - BS 1132 PN# 148A8310-3; PO# 816566 IAW SRM 51-40-02 AND IAW DWG# 148A8300