As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT NR 8 SLAT T/E WEDGE UPPER SURFACE METAL BOND REPAIR 58 INCHES FROM INBD END IS DEBONDED. REMOVED A 2INCH DIAMETER CORE AND ACCOMPLISHED PERMANENT REPAIR BONDED DOUBLER 5 INCH DIA AND CORE PLUG IAW 57-43-02, REPAIR 1, AND SRM 51-70-10, REPAIR 3, & 4.