As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PDX - 20K - LT FLAP PANEL 584EB HAS CHAF APPROX .020. BLENDED OUT DAMAGE IAW CRJ 700 SRM 57-52-02 PG 102. DAMAGE IS WITHIN LIMITS AND OK FOR CONTINUED SERVICE. ORIGINAL THICKNESS .100 MATERIAL REMAINING IS .078. PERFORMED FPI OF PANEL 584EB BLEND FOR CRACKS IAW CRJ 700 NDTM PART 01, 51-20-008. NO CRACKS NOTED. ETCHED, ALODINED AND PRIMED AFFECTED AREA.