As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT HORIZONTAL STAB LEADING EDGE HAS TOOL MARK AT APPROX 83 INCHES FROM INBD UPPER SIDE. DAMAGE REMOVED IAW SRM 51-10-02. ORIGINAL THICKNESS IS .040 REMAINING THICKNESS .030, MATERIAL LOSS .010 FOUND OUT OF LIMIT IAW SRM 55-10-01-1A-1. ACCOMPLISHED PERMANENT REPAIR IAW SRM 55-10-01-2R-1.