As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT HORIZONTAL STAB RIB AT STAB STA. 120.30 LOWER FLANGE AT 4TH STIFFENER CRACKED. ACCOMPLISHED HFEC SURFACE SCAN OF SUSPECTED CRACKED AREA IAW NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. MEASURED L 0.5'. ACCOMPLISHED HFEC INSPECTION OF OPEN HOLES OUTSIDE OF DAMAGED AREA IAW NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 16. NO CRACKS NOTED. REPAIRED THE STIFFENER IAW SRM 55-10-09-2R-5.