As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A TURBULENCE INSPECTION OF THE LEFT WING UPPER SURFACE, FOUND A THREE INCH CRACK ON FIXED PANEL AFT OF THE NR 7 SLAT. 12 INCHES INBD OF OTBD EDGE ON AFT EDGE OF PANEL. NO DEFORMATION AROUND CRACKED AREA. REMOVED AND REPAIRED THE PANEL IAW SRM 51-70-05, REPAIR .