As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C4 CHECK, NR 9 SLAT COVE PANEL BETWEEN OTBD MAIN TRACK LUG & AUX TRACK IS CRACKED AROUND FASTENER THAT MEASURED 2.125 INCH CRACK FROM COVE PANEL FASTENER, 2'6 INCHES FROM OTBD END & 1'1 INCH FROM TE. FABRICATED NEW COVE PANEL IAW DWG 141N4076. COMPLETED INSTALLATION OF COVE PANEL IAW DWG 114N4003 & SRM 51-10-02 PAR 9.