What was found
PDX- WING TO FUSELAGE JOINT STRAP IS CHAFED UNDER PANEL 92J. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B (1), PAGE 9 AND PARAGRAPH 3C (1-4) PAGE 8.
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 92J. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B (1), PAGE 9 AND PARAGRAPH 3C (1-4) PAGE 8.