As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PITTING AND CORROSION ON AFT MOUNTING PAD ON RT WING FOR NR 6 FLAP TRACK. REMOVED CORROSION IAW SRM 51-10-6 PG 5 FIG 4, FOUND TO BE WITHIN LIMITS ORIGINAL DRWG SPECS IAW DWG 66-14734. TREATED & PRIMED IAW SRM 51-10-2, ORIGINAL MAT THICKNESS .600, REMOVED .002 REMAINING .598.