As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
POTENTIAL TAILSTRIKE TAIL SKID PAD PER AMM TASK 05-51-32-202-025, 05-51-32-202-052, 05-51-32-202-038. SHOE DAMAGE WITHIN LIMITS. YELLOW CRUSH INDICATORS NOT SHOWING. SHOE BOLT HEAD TO TIP GAP IS 1.2 INCH THICKNESS. INTERIOR STRUCTURE HAS NO DAMAGE FOUND. OPERARION OF HORIZONTAL STABILIZER GOOD NO BINDING. TAKE OFF WARNING CHECK FOR STABILIZER GOOD. REPAINTED TAIL SKID TIP BLUE. AIRCRAFT BACK IN SERVICE.