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 O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA: 1.148' FINAL HOLE DIA: 1.163" MAXIMUM ALLOWABLE HOLE: 1.150" OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-04 AND EA 1-5750-T0342097 P1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.