What was found
CRACK ACCESS PANEL 321A LEADING EDGE RIB 8 ON VERTICAL STAB. REPLACED THE RIB AND FASTENERS AT IAW SRM 51-40-02-0G, DWG 174A0103, SHEET 13, REV-, & SRM 51-10-02-0G, STEP 9, ITEM A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ACCESS PANEL 321A LEADING EDGE RIB 8 ON VERTICAL STAB. REPLACED THE RIB AND FASTENERS AT IAW SRM 51-40-02-0G, DWG 174A0103, SHEET 13, REV-, & SRM 51-10-02-0G, STEP 9, ITEM A.