As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THIS INFO FOR FAA SDR. M/R HEAD DUE ERA SPINDLE INSPECTION. SINDLE SN A-356 HAD THREAD DAMAGE BEYOND LIMITS IAW 412-CR AND 0 CH. 62 (SCRAPPED) C/A: REMOVED SPINDLES AND VISUALLY INSPECTED ALL PARTS. C/W ERA SPINDLE INSPECTION AND TB 412-03-190. INSPECTED AND REASSEMBLED IAW 412-CR AND O CH 62 AND TB 412-03-190. PURGE LUBED ARM AND CLEVIS ASSEMBLY WITH OBIL 28 GREASE. REASSEMBLED WITH ORIGINAL SERVICEABLE BOLTS. COMPLIED WITH TB 412-03-190 ERA 412 SPINDLE INSPECTION.