As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENER LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02-0G; SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 154 REV - MEASURE OF CRACK IS :0.955 INCH.