What was found
DURING INSPECTION, VERTICAL STAB REAR SPAR CENTER HINGE FOR THE RUDDER FOUND CORRODED ON RT ATTACH LEG. REMOVED THE HINGE AND FOUND CORRODED LEG CRACKED. REPLACED HINGE IAW DAC MM 20-16-0, PG. 209, FIG. 205.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, VERTICAL STAB REAR SPAR CENTER HINGE FOR THE RUDDER FOUND CORRODED ON RT ATTACH LEG. REMOVED THE HINGE AND FOUND CORRODED LEG CRACKED. REPLACED HINGE IAW DAC MM 20-16-0, PG. 209, FIG. 205.