As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION APPROXIMATELY 1.5 INCH FOUND ON RIGHT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGES OF UPPER REAR SPAR CAPS AREA. REPAIRED AS PER SRM 55-20-00 FIGURE 3 VOLUME I REVISION 40. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100 REVISION 107. REPETITIVE INSPECTION REQUIRED, INITIAL AT 5400 CYCLES AND REPETITIVE INSPECTION AT 2700 CYCLES AS PER SRM 55-20-00 FIGURE 3 VOLUME I REVISION 40.