What was found
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 183 REV- DWG 143A5400 SHEET 182 REV-.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 183 REV- DWG 143A5400 SHEET 182 REV-.