What was found
INSPECTION FOUND FUSELAGE SKIN CORRODED WITH A BROKEN RIVET AT STA 680, STRINGER 26R. THE CORROSION WAS REMOVED AND THE CORRODED AREA WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-40-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CORRODED WITH A BROKEN RIVET AT STA 680, STRINGER 26R. THE CORROSION WAS REMOVED AND THE CORRODED AREA WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-40-5.