As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKED DRAG ANGLE RT LOWER VERT STAB (MARKED). PERFORMED EDDY CURRENT INSPECTION OF RT V/ STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE IS VERIFIED CRACKED AND END OF CRACK IS MARKED 9/4/08 VTJ7010159. GUT AWAY DAMAGED AREA OF RT DRAG ANGLE IAW RFO 670-55-31-018. (K)