What was found
HORIZONTAL ALTERNATE STAB TRIM - BELL CRANK -TAIL INTERIOR - BELL CRANK SUPPORT ROD END CORRODED. ROD END SURFACE CORROSION REMOVED PER AMM51-74-11. BOLT FROM RUDDER CONTROL ROD WAS NOT ADJUSTED OR DISCONNECTED
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HORIZONTAL ALTERNATE STAB TRIM - BELL CRANK -TAIL INTERIOR - BELL CRANK SUPPORT ROD END CORRODED. ROD END SURFACE CORROSION REMOVED PER AMM51-74-11. BOLT FROM RUDDER CONTROL ROD WAS NOT ADJUSTED OR DISCONNECTED