As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NUMBER 2 SLAT COVE SKIN IS CRACKED ADJACENT TO BOTH DRIVE TRACKS INBOARD OF ACCESS PANELS 524 CB AND OUTBOARD OF ACCESS PANELS 524 FB. STOPPED DRILLED CRACK AND INSTALLED EXTERNAL DOUBLER ON COVE SKIN INBOARD OF ACCESS PANEL 524 CB AND OUTBOARD OF ACCESS PANEL 524 FB PER AARD 57-43-04.