As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SKIN CRACKED, PREVIOUSLY STOP DRILLED CRACK AT BASE OF VERTICAL STAB FRONT SPAR, RT SIDE. REMOVED FASTENERS. CUT OUT DAMAGED SECTION OF SKIN. E/C INSP OK. FABRICATED FILLER AND BEGAN FABRICATION OF DOUBLER PER SRM 55-30-3. OK TO INSTALL DOUBLER. STARTED INSTALLING DOUBLER PER SRM 55-30-3. COMPLETED INSTALLATION OF DOUBLER PER SRM 55-30-3.