What was found
CORROSION ON RIB HOLES AT LT WING SLAT PANEL NR 4, STA XOS= 380. DAMAGE WAS REPAIRED IAW ETI-88-15-051 AND ER/A NR 532502-14, REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON RIB HOLES AT LT WING SLAT PANEL NR 4, STA XOS= 380. DAMAGE WAS REPAIRED IAW ETI-88-15-051 AND ER/A NR 532502-14, REV ORIGINAL.