What was found
INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 480, STRINGER 29L. THE STRINGER AND SPLICES WERE REMOVED AND THE SKIN CORROSION WAS CLEANED. STRINGER, SPLICE AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 480, STRINGER 29L. THE STRINGER AND SPLICES WERE REMOVED AND THE SKIN CORROSION WAS CLEANED. STRINGER, SPLICE AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 53-30-3.