As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN DAMAGE AT FR80/82 BETWEEN STR44LH AND STR 44RH VERIFIED THAT THE DAMAGE DUE TO THE TAIL STRIKE WAS REPAIRED IN ACCORDANCE WITH UPS EO-95523-REQ1, AIRBUS WORK CARD 7086636 AND AIRBUS REPAIR DRAWING R53970081 ISSUE B. REPAIR THRESHOLD IS TO BE TRACKED ON EO-95523-REQ2.