As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C CHECK - RT WING OTBD FLAP CHAFED THROUGH TOP COAT AT INBD END, UPPER SURFACE APPROX STA 192.0 TO 209.019. REMOVED CHAFE DAMAGE BY BLENDING IAW SRM 57-52-30-02-01, PARA 1-6B, STEPS 1-11. DIMENSIONS OF BLEND FOUND TO BE OUT OF LIMITS. HFEC AT BLENDED AREA FOR CRACK IAW NDTM PART 6, 51-00-01. NO CRACKS NOTED. MAPPED AREA FOR ENGINEERING. ALODINED, PRIMED AND PAINTED IAW RD 8/4-57-1416.