As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK SUPPORT ANGLE ON WING TO BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19R LOWER FUSELAGE. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON WING TO BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19R LOWER FUSELAGE IAW SRM 51-40-02 AND DWG 116A3118 SHEET 4 REV A ;DWG 116A3010 SHEET 33 REV C AND DWG 149A7101 SHEET 7 REV-.