As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1.5 INCH CRACK ON OUTBOARD SIDE AND A 1.5 INCH CRACK ON INBOARD DOUBLER OF NR 8 SLAT INBOARD ACTUATOR MOUNT AREA OF FRONT SPAR. THE INBOARD DOUBLER WAS REMOVED AND REPLACED AND THE OUTBOARD CRACK WAS STOP DRILLED IAW SRM 51-10-1.