As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WING L/E SLAT NR2 AFT INBD PANEL HAS A CRACK WITH STOP HOLE. CRACK STARTS FROM L/B MAIN TRACK ATTACHMENT AREA. ADJUSTMENT AND OPS TEST OF THE NR 2 L/E SLAT AFTER INSTALLATION CARRIED OUT AND FOUND GOOD IAW AMM 27-81-02, REV 5.2. THIS REPAIR IS CLASSIFIED AS MINOR RAW GMM 6-2-100 CRITERIA.