What was found
DURING SCHEDULED ROUTINE INSPECTION DISCOVERED CORROSION ON FUSELAGE APPROXIMATELY AT FS 243 TO 258 AT STRINGER 15L. REMOVED DAMAGED SKIN AND INSTALLED INSERTION REPAIR PATCH AND EXTERNAL DOUBLER REPAIR AND REPAIRED DAMAGED STR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED ROUTINE INSPECTION DISCOVERED CORROSION ON FUSELAGE APPROXIMATELY AT FS 243 TO 258 AT STRINGER 15L. REMOVED DAMAGED SKIN AND INSTALLED INSERTION REPAIR PATCH AND EXTERNAL DOUBLER REPAIR AND REPAIRED DAMAGED STR.