What was found
DURING C-CHECK, FOUND CRACKED ATTACH ANGLE AT VERTICAL STABILIZER WRAP AROUND PANEL. REPLACED ANGLE IAW DC9 SRM 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND CRACKED ATTACH ANGLE AT VERTICAL STABILIZER WRAP AROUND PANEL. REPLACED ANGLE IAW DC9 SRM 51-30-5.