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 FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 1.224", FINAL HOLE DIA 1.280", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341052 PART 1 STEP 2D AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.