What was found
LT MAIN GEAR RETRACT CYLINDER, UPON REMOVAL OF ACTUATOR ROD END, FOUND INTERNAL BORE THREADS CORRODED AND PITTED. *S/D* REMOVED AND REPLACED PER MM 32-33-20-4. WORK CARD 32 X 1702 14 OF 42 FOR INSTALL LT MAIN GEAR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT MAIN GEAR RETRACT CYLINDER, UPON REMOVAL OF ACTUATOR ROD END, FOUND INTERNAL BORE THREADS CORRODED AND PITTED. *S/D* REMOVED AND REPLACED PER MM 32-33-20-4. WORK CARD 32 X 1702 14 OF 42 FOR INSTALL LT MAIN GEAR.