As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) AN APPROX. 4 INCH CRACK WAS FOUND ON THE RT SIDE, UPPER REAR PORTION OF VERTICAL STAB. THE AREA IS JUST BELOW THE AFT LOWER FAIRING. THE AIRFRAME STRUCTURAL MANUAL CONTAINS A REPAIR SCHEME SPECIFIC TO THIS CRACKING. REF CHAP 55-00-00. REPAIRS ARE IN PROGRESS IAW SRM DRAWINGS. THE LOWER AFT FAIRING SHEAR FITTING AND PLATE ARE ALSO BEING REPLACED WITH NEW.