As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.222", FINAL HOLE DIA 1.252", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED & INST PER CMM 57-44-08 & EA 1-5750-T0342122 P1 STEP 2D & STEP 2. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.