What was found
DURING INSPECTION OF HORIZONTAL STAB PIVOT POINT FOR LUBE AND ISOLATION OF POPPING SOUND, FOUND ANTI-ROTATION FITTING CRACKED. AG TRIM WAS ADJUSTED CRACK WOULD OPEN AND POPPING WOULD ACCURE WHEN CRACK CLOSED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION OF HORIZONTAL STAB PIVOT POINT FOR LUBE AND ISOLATION OF POPPING SOUND, FOUND ANTI-ROTATION FITTING CRACKED. AG TRIM WAS ADJUSTED CRACK WOULD OPEN AND POPPING WOULD ACCURE WHEN CRACK CLOSED.