What was found
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 49 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 38, REV-. MEASUREMENT OF THE CRACK IS: 0.292 INCH.
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 49 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 38, REV-. MEASUREMENT OF THE CRACK IS: 0.292 INCH.