As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NOSE WHEEL WELL PANEL 113AC HAS CORROSION ON THE INSIDE FLANGE SURFACE AROUND FASTENER HOLES AS MARKED. / REMOVED CORROSION ON NOSE WHEEL PANEL 113AC INSIDE FLANGE DEEPEST BLEND AREA WAS .004 MATERIAL LOSS. SRM HAS NO LIMITS IN THIS AREA REPAIRED IAW AAR EA 180462 IR AND SWA EA 1-753-33199 REV IR