As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H WING LOWER LEADING EDGE PANEL 521CB IS DAMAGED ON THE INBOARD AFT CORNER. LOWER OUTER SKIN IS CRACKED 0.350 INCHES FROM INBOARD EDGE AND CRACK MEASURES 0.700 INCHES LONG.<[01] PERFORMED TIME LIMITED REPAIR ON PANEL 521CB IAW TSR 2023009725; ON FAULT TTG8Q00Q808E.;[02] PERFORMED TIME LIMITED REPAIR ON PANEL 521CB IAW TSR 2023009725 AND EA 23-157-03618; ON FAULT TTG8Q00Q808E.;[03] ADDED THE REFERENCE FOR THE DEFERRAL.