As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORROSION. BARREL NUT SURFACE REWORKED AS PER CMM 57-44-08 AND FOUND EXCEED LIMIT PER EA 1-5750-T0343585 P1 FIGURE 2. SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0343585 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.