What was found
PDX - CRACK ON VERTICAL STAB TO FUSELAGE LT CONNECTION ANGLE INTERMEDIATE SPAR II. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2 AND SRM 51-31-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PDX - CRACK ON VERTICAL STAB TO FUSELAGE LT CONNECTION ANGLE INTERMEDIATE SPAR II. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2 AND SRM 51-31-04.