What was found
CORROSION ON RT SLAT PANEL RIB OTBD FWD BORE AND INBD AFT BORE, XIS=40. DAMAGES WERE REWORKED AND MESURED WITH I.D. 0.940". FABRICATED AND INSTALLED BUSHINGS 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 RT SLAT PANEL RIB OTBD FWD BORE AND INBD AFT BORE, XIS=40. DAMAGES WERE REWORKED AND MESURED WITH I.D. 0.940". FABRICATED AND INSTALLED BUSHINGS IAW SRM 57-02, PAR 9.