As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING LEADING EDGE CAVITY PANEL SUPPORT ANGLE IS CRACKED, OUTBD OF THE NR 8 SLAT TRACK. REMOVED FORMER IAW SRM 51-35-01 & 51-33-01; VOL II. FABRICATED PER DWG ARB1162, REV "S". ALODINED & PRIMED IAW SRM 51-21-01; VOL II; PGS 21 - 24. INSTALLED IAW SRM 51-35-01 & 51-33-01; VOL II.