What was found
CRACK ON RIB 8 OF ACCESS PANEL 321A AT VERTICAL STABILIZER. REPLACED RIB 8 OF ACCESS PANEL 321A AT VERTICAL STABILIZER AND FASTENERS IAW SRM 51-40-02 AND 51-10-02 ITEM 9 AND DWG 174A 0103 SHEET 1 REV -.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON RIB 8 OF ACCESS PANEL 321A AT VERTICAL STABILIZER. REPLACED RIB 8 OF ACCESS PANEL 321A AT VERTICAL STABILIZER AND FASTENERS IAW SRM 51-40-02 AND 51-10-02 ITEM 9 AND DWG 174A 0103 SHEET 1 REV -.