What was found
LT FWD VERTICAL STAB-TO-FUSELAGE REENFORCEMENT ANGLE CRACKED ON AFT END. REMOVED CRACKED LT FWD VERTICAL STAB-TO-FUSELAGE REINFORCEMENT ANGLE, PREPPED AND INSTALLED SERVICEABLE ANGLE IAW AEA EO EM-53MR-1281.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT FWD VERTICAL STAB-TO-FUSELAGE REENFORCEMENT ANGLE CRACKED ON AFT END. REMOVED CRACKED LT FWD VERTICAL STAB-TO-FUSELAGE REINFORCEMENT ANGLE, PREPPED AND INSTALLED SERVICEABLE ANGLE IAW AEA EO EM-53MR-1281.