What was found
RT VERTICAL TO FUSELAGE DRAG ANGLE HAS A CRACK. REMOVED AND REPLACED DRAG ANGLE P/N AV670-71186-003 IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, AND DRAWING BA670-30100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT VERTICAL TO FUSELAGE DRAG ANGLE HAS A CRACK. REMOVED AND REPLACED DRAG ANGLE P/N AV670-71186-003 IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, AND DRAWING BA670-30100.