What was found
DURING C-CHECK, FOUND THE VERTICAL STABILIZER TO FUSELAGE LEFT ATTACH ANGLE CRACKED. REMOVED AND REPLACED THE ANGLE IAW DC-9 SRM 53-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND THE VERTICAL STABILIZER TO FUSELAGE LEFT ATTACH ANGLE CRACKED. REMOVED AND REPLACED THE ANGLE IAW DC-9 SRM 53-05.