As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT I/B HOLE BORE FOUND WITH CORROSION. AFT HINGE (FLAP SIDE) PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341083 PART 1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.