As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE FUSELAGE BELLY SKIN AT FS 213.25 AND STRINGER 15R CORRODED IN AN AREA OF 1" BY .75". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-044 MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.