What was found
DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED MINOR CORROSION APPROXIMATELY FS 250 AT STRINGER 15L. REMOVED DAMAGED FUSELAGE SKIN AND INSTALLED INSERTION AND EXTERNAL DOUBLER REPAIRS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED MINOR CORROSION APPROXIMATELY FS 250 AT STRINGER 15L. REMOVED DAMAGED FUSELAGE SKIN AND INSTALLED INSERTION AND EXTERNAL DOUBLER REPAIRS.