As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT I/B FORE FLAP LOWER SKIN SURFACE T/E CHAFED AT WBL 123. REMOVED DAMAGED SKIN, CLEANED AREA, FABED REPAIR PARTS HF/ALODINED AND APPLIED BONDING PRIMER TO BOND SURFACES AND INSTALLED REPAIR PARTS WITH METAL TO METAL HOT BOND; CURED AT 225-250 DEGREES FOR 90 MIN; ALL IAW SRM 51-53-02 AND 51-70-10 REPAIR 18.