As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING SHOP INSPECTION, THE 4TH RIB FOR I/B END WAS FOUND CRACKED. THE RIB WAS REPAIRED PER SRM 57-54-00. THE LOWER COVE PANEL ATTACH ANGLE UNDERNEATH THE I/B UPSTOP WAS FOUND TO HAVE A CRACK. THE ANGLE WAS REPAIRED PER SRM 57-54-0 FIG 812, FOR NR 2 L/E SLAT.