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 31 INCHES FROM INBD END IS DEBONDED. REMOVED A 2 INCH DIA CORE AND ACCOMPLISHED PERMANENT REPAIR BONDED DOUBLER 5 INCHES IN DIAMETER AND CORE PLUG IAW SRM 57-43-02, REPAIR 1, AND SRM 51-70-10 REPAIR 3 AND 4.