What was found
DURING INSPECTION, THE RT REAR FUSELAGE SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 65 AND FRAME 68. THE SILL WAS REPLACED IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, THE RT REAR FUSELAGE SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 65 AND FRAME 68. THE SILL WAS REPLACED IAW SRM 51-40-02.