As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT I/B FLAP HAS AN AREA OF DELAMINATION ON UPPER SURFACE, WS 275 CUT OUT DELAMINATED AREA 7 1/2 INCH BY 7 1/2 INCH ON LT I/B FORG FLAP UPPER SURFACE AND REMOVED DAMAGED CORE 7 1/2 BY 7 1/2. SHAPED SECTION OF CORE 7 1/2 INCH BY 7 1/2 INCH. FABRICATED DOUBLER 10 1/2 INCH BY 10 1/2 INCH. BONDED CORE PLUG AND DOUBLER, CLEANED, PRIMED AND SEALED IAW SRM 51-40-24 FIG 1.