As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TAIL STRIKE DAMAGE WAS FOUND TO THE LOWER BELLY SKIN. FOUND CORROSION ON EXTERNAL SKIN, AROUND FASTENERS AND CENTER DRAIN HOLE AT BS 1720, S29L TO S29R. N/R 58 Z100 WRITTEN. MEASUREMENT OF DOUBLER THICKNESS IS UNIFORM .075" DOUBLER IAW EA55-32034 IAW SRM.