As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKED DRAG ANGLE LEFT LOWER VERT STAB (MARKED). PERFORMED EDDY CURRENT INSPECTION OF LEFT V/STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE IS VERIFIED CRACKED AND END OF CRACK IS MARKED. PERFORMED CUTOUT OF DAMAGED AREA LOCATED OF LT LOWER VERTICAL STAR AND REMOVED BURS AND SHARP EDGES IAW RFO 670-55-31-018. (K)