As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT MLG SHOCK STRUT (OUTER CYLINDER) LOWER CURCUMFERENTIAL INTERNAL THREADS ARE CORRODED/PITTED. ALSO, THE SHOCK STRUT GLAND NUT THREADS FOR MLG OUTER CYLINDER (SHOCK CYLINDER) ARE CORRODED/PITTED (REF SNRM 872). RIGHT MAIN OUTER CYL.-LOWER CIRCUMFERENTIAL INTERNAL THREAD CORROSION ON MLG CYL. PART IS NOT ACCEPTABLE FOR CONTINUED SERVICE. GEAR REPLACED PER WORKCARD 32T1701-RC, SEQ. 000879.