As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING LEFT HAND WING OUTBOARD FLAP INBOARD FORWARD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08 AND FOUND EXCEED LIMIT. BASE THE DIFFERENCE BETWEEN DRAWING LIMIT AND CMM MAX REWORK LIMIT. SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-130948A P2 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.