What was found
CORROSION ON RIB HOLES AT RT SLAT PANEL, NR 0, XFS 40. CORROSION ON RIB HOLES AT RT SLAT PANEL WAS REPAIRED IAW SRM 57-02, PAR 9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON RIB HOLES AT RT SLAT PANEL, NR 0, XFS 40. CORROSION ON RIB HOLES AT RT SLAT PANEL WAS REPAIRED IAW SRM 57-02, PAR 9.