As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C1, LT WING INBD FLAP TOP SURFACE IS GOUGED OUTBOARD END, BLENDED AREA IAW A300 SRM 57-50-00. ORIGINAL THICKNESS OF .032 REMAINING MATERIAL .025 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE IAW A300 SRM 51-50-00 INSTALLED REPAIR DOUBLER IAW A300 SRM 51-21-00 & 51-40-40.