As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT VERTICAL STAB DRAG ANGLE CRACKED AT AFT END (MARKED). PERFORMED EDDY CURRENT INSPECTION OF LT VERTICAL STAB DRAG ANGLE IAW NDTM 51-20-006 TO LOCATE END OF CRACK. END OF CRACK IS MARKED. INSTALLED AND SEALED L/H DRAG ANGLE PER REO 670-55-31-018.