What was found
PDX- WING TO FUSELAGE JOINT STRAP IS CHAFED UNDER PANEL 91J. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B STEP 2 AND PARAGRAPH 3C STEPS 1 THRU 4 AND HORIZON AIR EA 4-53-376.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PDX- WING TO FUSELAGE JOINT STRAP IS CHAFED UNDER PANEL 91J. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B STEP 2 AND PARAGRAPH 3C STEPS 1 THRU 4 AND HORIZON AIR EA 4-53-376.