What was found
CRACK ON ANGLE WING TO BODY FARING STRUCTURE BS 500D AT LEVEL STR19L AT LOWER FUSELAGE. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 116A3010, SHEET 39, REV-.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON ANGLE WING TO BODY FARING STRUCTURE BS 500D AT LEVEL STR19L AT LOWER FUSELAGE. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 116A3010, SHEET 39, REV-.