As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STAB TO FUSELAGE LH FWD DRAG ANGLE IS CRACKED AT REAR SPAR DATUM 67.5%. (C-CHECK RO 7/10/2021) REPAIRED VERTICAL STAB TO FUSELAGE LH FWD DRAG ANGLE IAW REO 670-55-31-018 REV A, DATED 2013-11-10. COMPLETED MAJOR REPAIR FORM 337 AND TASK CARD 51-900-1002-SKY, +0.2 LB CHANGE TO WEIGHT