As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD PIT STA 500I SIDEWALL SUPPORT ANGLE CORRODED AT LBL24 AND WL157 / REMOVED CORROSION FROM STA 500I BULHEAD SPPORT ANGLE AT LBL 24 ORIGINAL MATERIAL THICKNESS .071 LOSS OF .008 WITH .063 REMANING IS OUT OF LIMITS DUE TO NO PUBLISHED LIMITS ACCOMPLISHED AAR EA 200487 REV IR AND SWA WORK INSTRUCTIONS 20-153-01904 REV IR TO LEAVE AS IS. P/N 143A9485-23