As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND 200 AREAS OF CORROSION ON INNER THRESHOLD PANELS. REMOVED PAINT FROM SUSPECT AREAS ON INNER THRESHOLD PANELS AND FOUND 180 AREAS THAT WERE BEYOND SURFACE CORROSION. MATCH DRILLED AND TRIMMED NEW FWD(P/N: 6911084-11), CENTER(P/N: 6911084-5), AFT(P/N: 6911084-12) INNER THRESHOLD SKINS.