As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1 INCH CRACK IN AFT MOST LEFT RIB AT FASTENER HOLE OF VERTICAL STABILIZER SADDLE FAIRING. THE RIB WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-2 AND 55-01. A DOUBLER AND RIB WERE INSTALLED IAW SRM 55-01, 51-30-2, AND 51-30-5.