As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NOSE WHEEL WELL PANEL 114 BW HAS CORROSION ON INNER UPPER SURFACE AT FASTENER HOLES; MARKED. / REMOVED CORROSION FROM NOSE WHEEL WELL PANEL 114BW ON INNER UPPER SURFACE ORIGINAL 'T' .192'; REMOVED .007'; .185' REMIANING BOEING FINDS IT TO BE STRUCTURELY ACCEPTABLE; RESTORED SURFACE FINISH IAW EA 1-753-33228 REV IR AND EA 180490 IR