What was found
LEFT AFT VERT STAB TO FUSELAGE DRAG ANGLE HAS A 1" CRACK ON LEADING EDGE.-C/A-REPAIRED LEFT DRAG ANGLE IAW 55-31-00-201-001-A01
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT AFT VERT STAB TO FUSELAGE DRAG ANGLE HAS A 1" CRACK ON LEADING EDGE.-C/A-REPAIRED LEFT DRAG ANGLE IAW 55-31-00-201-001-A01