As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT OTBD FLAP BOTTOM SKIN HAS A CLUSTER OF SHARP DENTS JUST INBD OF VANE ROLLER ACCESS PANEL 557DB. INSPECTED DAMAGE AREA FOUND TO BE SERIES OF GOUGE SHARP CREASE DENTS TO INCLUDE ONE LOSE FASTENER - OUT OF LIMITS IAW SRM 57-10-00 PG 162A TO 48, HFEC DENT IAW NTSPM 06-10-01 NO CRACK FOUND. FABRICATED REPAIR DOUBLER IAW SRM 57-10-00, FIG 85, INSTALLED REPAIR DOUBLER IAW SRM 51-31-01, RSC TRACKING EA 8-5750-163986. MAJOR REPAIR.