What was found
RIGHT VERTICAL STAB CONNECTION ANGLE AT FRONT SPAR (16 PERCENT) IS CRACKED. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT VERTICAL STAB CONNECTION ANGLE AT FRONT SPAR (16 PERCENT) IS CRACKED. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.