What was found
PDX - THREE CRACKS IN SKIN PANEL BENEATH THE LEADING EDGE OF THE RUDDER ON THE LT SIDE AT THE STIFFENER. REPAIRED IAW FOKKER SRM 53-02-05, PAGE 10, FIGURE 5 AND SRM 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PDX - THREE CRACKS IN SKIN PANEL BENEATH THE LEADING EDGE OF THE RUDDER ON THE LT SIDE AT THE STIFFENER. REPAIRED IAW FOKKER SRM 53-02-05, PAGE 10, FIGURE 5 AND SRM 51-31-01.