What was found
AFT DRAG ANGLE ON RT SIDE OF VERTICAL STAB IS CRACKED APPROXIMATELY .5 INCH. REMOVED AND REPLACED AFT DRAG ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT DRAG ANGLE ON RT SIDE OF VERTICAL STAB IS CRACKED APPROXIMATELY .5 INCH. REMOVED AND REPLACED AFT DRAG ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.