As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SUPPLEMENTAL: REPORT: LH AFT MAIN LANDING GEAR BODY PANELS AND PROTION OF FUSELAGE DAMAGE DUE TO TUG CONTACT WITH AIRCRAFT. CORRECTIEV ACTION: REPAIRED LEFT AFT MAIN LANDING GEAR BODY PANLES AND FUSELAGE DAMAGE IAW EO ATR42-5300-2021-001 AND ATR INSTRUCTION REFERENCE ES-0148580-02 ISSUE C.