What was found
CORROSION ON RIB HOLES XOS= 610 AT LT WING SLAT PANEL NR 5. CORROSION ON RIB HOLES STA XOS= 610 AT LT WING SLAT PANEL NR 5 WAS REMOVED, REPAIR BUSHINGS WERE FABRICATED AND INSTALLED 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 XOS= 610 AT LT WING SLAT PANEL NR 5. CORROSION ON RIB HOLES STA XOS= 610 AT LT WING SLAT PANEL NR 5 WAS REMOVED, REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 57-02, PAR 9.