As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND ON CV2 CHECK 1.) 1.25 INCH CRACK AT NR 7 SLAT COVE PANEL ATTACH ANGLE JUST INBOARD OF INBOARD TRACK. 2.) SCREWS/BOLTS LOOSE AT NR 7 SLAT INBOARD TRACK FAIRING. REPAIR: 1.) REPAIRED PER M/M 57-54-0 PAR 2. 2.) REPAIRED AS SECURED FASTENERS.