As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT VERTICAL STAB LOWER DRAG ANGLE CRACKED (MARKED). CRACK LENGTH WAS VERIFIED IAW SRM NDTM 51-20-006. LEFT VERTICAL STAB TO FUSELAGE DRAG ANGLE REPAIRED BY COMPLIANCE WITH EC/TC REO 670-55-31-018 IAW REO 670-55-31-018 FOR LEFT SIDE ONLY. RESTORED PROTECTIVE COATING AT REPAIR AREA PER SRM 51-25-01. REFERENCE THE FOLLOWING STEPS OF THIS TASK CARD AND WORK ORDER 111462 EC/TC REO 670-55-31-018 FOR SIGN-OFFS OF INDIVIDUAL TASKS ACCOMPLISHED.