As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PDX - C1 - FUSELAGE FAIRING PANEL 261CT HAS CHAFING ALONG FWD EDGE UNDERSIDE MATING SURFACE. BLENDED DAMAGED AREA MAX MATERIAL REMOVED .003" , IAW RD 8/4-53-521 STEP 1-2. HFEC AREA IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ALODINED AND PRIMED REPAIR AREAS IAW RD 8/4-53-521 STEP 4-8.