As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT MLG SHOCK STRUT (OUTER CYLINDER) LOWER CIRCUMFERENTIAL INTERNAL THREADS ARE CORRODED/PITTED. ALSO, THE SHOCK STRUT GLAND NUT THREADS FOR MLG OUTER CYLINDER (SHOCK STRUT) ARE CORRODED/PITTED. LT MAIN OUTER CYL.-CIRCUMFERENTIAL INTERNAL THREAD CORROSION ON MLG CYL. PART IS NOT ACCEPTABLE FOR CONTINUED SERVICE. GEAR REPLACED PER WORKCARD 32T1701-LC, SEQ. 000878.