As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) CRACK LOCATED ON THE REAR FACE OF THE LT STAB ATTACH BRACKET, THE CRACK PARALLELS THE OB ATTACH FLANGE (ANCHOR NUT ATTACH SIDE) FOR 1.3750. THE CRACK HAD STARTED AT THE TOP OF THE STAB ATTACH BRACKET AND HAD WORKED ITS WAY DOWN. THE CRACK ON THE BRACKET WAS ONLY VISIBLE ONCE THE BRACKET WAS REMOVED FROM THE FRONT SPAR FOR SPECIAL INSPECTION CF-91-42.