As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. I/B ACTUATOR LUG HOLE REMOVED CORROSION AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.221 AND REPAIRED AS PER FEDEX EA 1-5750-74315. LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.