What was found
VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT BSTA 1542-1587. REPAIRED IAW TECHNICAL ORDER PAM-TO-51-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT BSTA 1542-1587. REPAIRED IAW TECHNICAL ORDER PAM-TO-51-10.