What was found
VERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED, LEFT SIDE OF VERTICAL AFT END. REPAIRED ANGLE IAW DC-9 SRM 53-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED, LEFT SIDE OF VERTICAL AFT END. REPAIRED ANGLE IAW DC-9 SRM 53-05.