As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B PIVOT HOLE BORE FOUND WITH CORROSION. CORRODED PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.124". FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T034101B PT 1 STEP 1A. REPAIR CLASSIDFIED MINOR PER GMM 6-2-100.