What was found
VERTICAL STAB RT, HAD CORROSION BELOW UPPER RUDDER ACTUATOR. REMOVED CORROSION AND BLEND OUT IAW EA 8-5530-T0333328 P1, SRM 51-21-01, VOL II, SRM 51-21-02, VOL II, PGS 2-9, SOPM 20:10.10, PG 25, AND DPS 2.50.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STAB RT, HAD CORROSION BELOW UPPER RUDDER ACTUATOR. REMOVED CORROSION AND BLEND OUT IAW EA 8-5530-T0333328 P1, SRM 51-21-01, VOL II, SRM 51-21-02, VOL II, PGS 2-9, SOPM 20:10.10, PG 25, AND DPS 2.50.