As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PDX - 20K - RT FLAP PANEL 684EB HAS CHAF. BLENDED OUT DAMAGE IAW CRJ SRM 57-52-02 PG 102 AND FOUND TO BE WITHIN LIMITS. ORIGINAL THICKNESS .100 REMAINING IS .085 OK FOR SERVICE. FPI BLENDED AREA FOR CRACKS IAW SRM 51-12-00-001-001-A01 PAGE 10, PAR 7B(4), AND CRJ NDTM PART 1, 51-20-008. NO CRACKS NOTED. ETCHED, ALODINED AND PRIMED AFFECTED AREA.