What was found
CORROSION ON RIB HOLE, STA XIS=136 AT LT WING SLAT PANEL 1. CORROSION ON RIB HOLE STA 136 WAS REMOVED, WAS FABRICATED BUSING AND INSTALLED IAW SRM 57-02, PAR. 9C, 1, 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON RIB HOLE, STA XIS=136 AT LT WING SLAT PANEL 1. CORROSION ON RIB HOLE STA 136 WAS REMOVED, WAS FABRICATED BUSING AND INSTALLED IAW SRM 57-02, PAR. 9C, 1, 2.