As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF RUBSTRIP ON NR N00391 RT WING OTBD FLAP UPPER MAIN SKIN BETWEEN RIBS 4 AND 5 ALSO BETWEEN THE MAIN SPAR CHORD AND REAR SPAR CORD HAS 8 DENTS WHICH 2 EA ARE VISABLE UNDER THE RUBSTIPS. DAMAGE IS IN A 10 IN X 12 IN AREA. CUTOUT DAMAGE AREA AND REPAIRED IAW SRM 57-53-12, PARA 14, PG 255-260, FIG 210 C/W EA 6-5750-145550.