What was found
REPLACE R/H WING I/B FLAP O/B AFT FLAP HINGE DUE TO HEAVY CORROSION VERIFIED STEP 11 IS C/W AND AUDIT C/W. REMOVE AND REPLACE INBOARD FLAP OUTBOARD HINGE ASSEMBLY P/N ARC2512-504 PER CMM 57-52-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
REPLACE R/H WING I/B FLAP O/B AFT FLAP HINGE DUE TO HEAVY CORROSION VERIFIED STEP 11 IS C/W AND AUDIT C/W. REMOVE AND REPLACE INBOARD FLAP OUTBOARD HINGE ASSEMBLY P/N ARC2512-504 PER CMM 57-52-03.