As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT O/B FLAP I/B AFT HINGE PIVOT I/B HOLE BORE FOUND WITH CORROSION. AFT HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.149", FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341020 PART 1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.