What was found
INSPECTION FOUND FUSELAGE SKIN CORRODED BETWEEN STA 715 AND 725 AT STRINGER 13L. THE CORRODED AREA WAS REMOVED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-01 AND 51-33-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CORRODED BETWEEN STA 715 AND 725 AT STRINGER 13L. THE CORRODED AREA WAS REMOVED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-01 AND 51-33-01.