As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STABILIZER ATTACH FITTING AT RIB 12 HAS CORROSION. REMOVED CORROSION PER SRM 51-74-10. APPLIED ALODINE TO THE REWORKED AREA PER SRM 51-21-10. FREE OF CRACK AT THE REWORKED AREA. REMAINING THICKNESS IS 0.481 INCH, IT IS WITHIN LIMIT PER SRM 55-30-00/101 CONFIG 1. RESTORED FINISH AND CIC THE REWORKED AREA PER SRM 51-75-10 AND SRM51-23-20.