What was found
LEFT SIDE, VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE HAS A 1 1/2" CRACK ALONG LEADING EDGE.-C/A-REPAIRED IAW SRM 55-31-00-995-801
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT SIDE, VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE HAS A 1 1/2" CRACK ALONG LEADING EDGE.-C/A-REPAIRED IAW SRM 55-31-00-995-801