What was found
RIGHT AFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE WAS CRACKED. 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.
RIGHT AFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE WAS CRACKED. REPAIRED ANGLE IAW DC-9 SRM 53-05.