As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FAULT - STIFFENER CENTER WING FRONT SPAR CRACK IS STIFFENER AT STA 785.9 LBL 33 (REPAIR) PERFORM REPAIR I.A.W SRM 57-10-10-2R-2 REPAIR INSTRUCTIONS 4.O~Q REV.86 AND SREO-58151-REQ001 REV.1 AND SREO-76672-REF REV.1 BOEING DWG NO.111T5202 SH.2 REV.- AND BOEING DWG NO.140T0520 SH.23 REV.-. STIFFENER CENTER WING FRONT SPAR CRACK IS STIFFENER AT STA 785.9 LBL 33 (REPAIR) REVIEWED