What was found
PDX- OBLIQUE FRAME TO FUSELAGE CLIP AFT OF FRAME 32-2 AT STRINGER 48 HAS A CRACK. REPAIRED IAW FOKKER SRM 53-10-05 PAGE 601 AND SRM 53-02-13, PAGE 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PDX- OBLIQUE FRAME TO FUSELAGE CLIP AFT OF FRAME 32-2 AT STRINGER 48 HAS A CRACK. REPAIRED IAW FOKKER SRM 53-10-05 PAGE 601 AND SRM 53-02-13, PAGE 5.