As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-16 CHECK THE UPPER SURFACE OF THE RT INBOARD FORE-FLAP WAS FOUND DISBONDING 33 INCH TO 37 INCH FROM THE OUTBOARD END. MAINTENANCE PERFORMED HONEYCOMB CORE REPAIR ON RT INBOARD FORE-FLAP IAW B737-200 SRM 51-40-20, REPAIR NR 9, FIG. 18, PG. 63-67.