What was found
CRACK ANGLE FLOOR STRUCTURE BTW STA 380 TO STA 400 AND LBL 13 AT PASSENGER CABIN. REMOVE AND REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, DWG 143A5400, SHT 182, REV -, DWG 143A5400, SHT 184, REV-.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ANGLE FLOOR STRUCTURE BTW STA 380 TO STA 400 AND LBL 13 AT PASSENGER CABIN. REMOVE AND REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, DWG 143A5400, SHT 182, REV -, DWG 143A5400, SHT 184, REV-.