What was found
CORROSION ON FLAP HINGE SUPPORT STA XW 251 AT LEFT WING REAR SPAR. LT WING FLAP HINGE SUPPORT FITTING WAS REPAIRED, BUSHING WERE FABRICATED AND INSTALLED PER CMM 27-50-5 PAR 2 I AND HINGE WAS INSTALLED PER AMM 57-40-01-201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FLAP HINGE SUPPORT STA XW 251 AT LEFT WING REAR SPAR. LT WING FLAP HINGE SUPPORT FITTING WAS REPAIRED, BUSHING WERE FABRICATED AND INSTALLED PER CMM 27-50-5 PAR 2 I AND HINGE WAS INSTALLED PER AMM 57-40-01-201.