As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING WALK AROUND FOUND SUSPECTED CRACK IN RT WING AROUND SLAT DRIVE MECHANISM ACCESS DOOR. HFEC INSPECTED CRACK INDICATED IAW SOPM 20-30-00. REMOVED DAMAGE IAW SRM 57-40-02 REPAIR 7. PERFORMED HFEC OF CUT OUT AREA ON RT WING TO ENSURE CRACK REMOVAL IAW NTM PT6. FABRICATED REPAIR PARTS IAW SRM 57-40-02 FIG 202. REPAIRED RT WING SLAT DRIVE ACCESS DOOR IAW SRM 57-40-02 REPAIR 7.