As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND HOLES HAVE EVIDENCE OF PITTING. REMOVED PITTING AND CORROSION FROM LUG AND BORE. FABBED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW SRM 57-20-00 VOL. I PAGE 16. BLENDED FLAT SPOTTED AREA IAW EA8-5750-81494. ORIGINAL LUG THICKNESS WAS 1.015 INCH FINAL LUG THICKNESS .990 INCH. SEE NR N01176