What was found
CRACK RIB 8 ON ACCESS PANEL 321A AT VERTICAL STABILIZER. REPLACED THE RIB IAW SRM 51-40-02, SRM 51-1002, ITEM 9, DWG 147A1008, SHEET 1, REV B, & DRAWING 174A0103, SHEET 1, REV -.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK RIB 8 ON ACCESS PANEL 321A AT VERTICAL STABILIZER. REPLACED THE RIB IAW SRM 51-40-02, SRM 51-1002, ITEM 9, DWG 147A1008, SHEET 1, REV B, & DRAWING 174A0103, SHEET 1, REV -.