What was found
LT HORIZONTAL STAB UPPER REAR SKIN PANEL CRACKED, INITIATING FROM AFT EDGE OF SKIN AND PROCEDING FWD 21/4" (APPROXIMATELY). VERIFIED BY HFEC INSPECTION MARKED END OF CRACK. COMPLIED WITH AE 8-5510-116939. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT HORIZONTAL STAB UPPER REAR SKIN PANEL CRACKED, INITIATING FROM AFT EDGE OF SKIN AND PROCEDING FWD 21/4" (APPROXIMATELY). VERIFIED BY HFEC INSPECTION MARKED END OF CRACK. COMPLIED WITH AE 8-5510-116939. MAJOR REPAIR.