What was found
FWD FUSELAGE INTERNAL, LT SILL PLATE CORRODED BETWEEN FR 12-16 LBL 46. THE SILL PLATE WAS REPLACED WITH NEW PART IAW SRM 51-43-03 AND 51-41-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FWD FUSELAGE INTERNAL, LT SILL PLATE CORRODED BETWEEN FR 12-16 LBL 46. THE SILL PLATE WAS REPLACED WITH NEW PART IAW SRM 51-43-03 AND 51-41-02.