What was found
CORROSION ON RIB XOS=83 AND HOLES XOS=166 AT LT WING SLAT PANEL NR 1. CORROSION ON HOLES RIB BS XOS=83 AND XOS=166 AT LT WING SLAT PANEL NR 1 WAS REMOVED 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 XOS=83 AND HOLES XOS=166 AT LT WING SLAT PANEL NR 1. CORROSION ON HOLES RIB BS XOS=83 AND XOS=166 AT LT WING SLAT PANEL NR 1 WAS REMOVED IAW SRM 57-02, PAR 9.