As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STABILIZER RIB, HAS A GOUGE ON THE TOP SURFACE BEHIND L/E PANEL. BLENDED DAMAGE TO SMOOTH CONTOUR AND FOUND TO BE WITHIN LIMITS. NDT REPORTED NO DEFECTS. ROTO PEENED TO 200 PERCENT INTENSITY AND RESTORED THE FINISH. WORK DONE IAW EA.