As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SBN - UPPER ATTACHMENT ANGLE ON THE VERTICAL STABILIZER AT THE LOWER RUDDER HINGE POINT IS CRACKED AT RIB 29.53. MAINTENANCE FABRICATED ANGLE PER SAMPLE AND INSTALLED. ALL WORK WAS DONE IAW BAE SRM 55-30-00, 51-30-01, AND 51-10-06. (M)