What was found
THE FUSELAGE SKIN WAS FOUND CORRODED AT THE S-26L LAP SPLICE AT STA 575. THE SKIN DAMAGE IS ADJACENT TO A PREVIOUSLY INSTALLED INTERNAL REPAIR. THE NEW DAMAGE WAS REPAIRED WITH AN OVERLAPPING DOUBLER PER ER/A 363252-14, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE SKIN WAS FOUND CORRODED AT THE S-26L LAP SPLICE AT STA 575. THE SKIN DAMAGE IS ADJACENT TO A PREVIOUSLY INSTALLED INTERNAL REPAIR. THE NEW DAMAGE WAS REPAIRED WITH AN OVERLAPPING DOUBLER PER ER/A 363252-14, REV A.