What was found
LEFT VERTICAL TO FUSELAGE DRAG ANGLE CRACKED AT APPROXIMATELY FRAME 76. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT VERTICAL TO FUSELAGE DRAG ANGLE CRACKED AT APPROXIMATELY FRAME 76. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-40-02.