What was found
CORROSION ON RIB HOLES XIS=136.42 ON LT WING SLAT PANEL. RIB 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 XIS=136.42 ON LT WING SLAT PANEL. RIB REPAIRED IAW SRM 57-02, PAR 9.