As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/W LOWER LEADING-EDGE PANEL#521XB HAS SCREW HOLE CRACKED. 8-46<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #521XB AS PER B737 SRM 51-70-04-2R-9; MATERIAL USED; PO#1791128; PO#1473815; TOOL USED; TEMP CONTROLLER ID 160354; CALIBRATION DUE 03-07-25.;[02] VERIFIED STEP 1<BR>AUDIT PER MPM 52-02-02