As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT INBOARD FLAP VANE TOP SURFACE 6 INCHES INBOARD FROM OUTBOARD HOIST POINT IS AN AREA GOUGED AND WORN 2 X 2.5 X .012 INCH (BEEN CHAFING ON NR 2 SPOILER ACTUATOR DRIP PAN). BLENDED OUT DAMAGE IAW SRM 51-73-10. NDT BLENDOUT IAW NTM 51-10-08. FILLED REWORK AREA WITH EA 934 A&B IAW EA 6-5750-69671. FABRICATED AND INSTALLED BONDED STEEL DOUBLER PER SRM 57-52-12 FIG 202 AND FAX 942-023683/005/2003 AND EA 6-5750-69671.