As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION FOUND ON INNER FUSELAGE BELLY SKIN 2 INCHES FWD OF BS 265 RIGHT NEXT TO STR 27. COMPLIED REO 670-53-11-2208, REV-. DISPOSITION FOR BLENDED CORROSION DAMAGE TO FUSELAGE SKIN PANEL NEAR BS 265 BTWN STR 26R-STR27. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1, 51-20-006 AND NDTM PART 6, 51-00-001 AND ENSURED REWORKED AREAS ARE CRACK FREE.