As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT OUTBOARD AFT FLAP LOWER SKIN TRAILING EDGE WEDGE HAS DELAMINATED DENT APPROXIMATELY 2 INCHES IN DIAMETER, 21 INCHES FROM OUTBOARD END OF FLAP AND 4.5 INCHES FROM TRAILING EDGE. REMOVED DELAMINATED SKIN AND CORE TO 0.5 DEPTH. BONDED IN NEW CORE PLUG. HOT BONDED GRAPHITE PRE-PREG LAY-UP PERMANENT REPAIR OVER CORE PLUG PER SRM 51-70-04-0G.