As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
#5 SLAT SKIN CRACKED AT ACTUATOR ATTACH POINT. #5 SLAT SKIN CRACK END POINT MARKED AND VISUALLY MEASURED AT 7/16". #5 SLAT HAS BEEN REMOVED. COMPLETED INTERFACE INSPECTION ON #5 SLAT, OK TO INSTALL. INSTALLED #5 SLAT. N/R REMAINS OPEN FOR RIGGING. RII ACCOMPLISHED ON #5 SLAT INSTALLATION. RT WING LEADING EDGE SLATS RIGGED.