As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H UPPER APRON PANEL 333AT AT FUSELAGE AREA, SUPPORT FITTING HAS A CRACK. MARKED AREA. REMOVED ACCES L/H UPPER APRON PANEL 333AT AND 331AB AT FUSELAGE AREA TO GAIN ACCESS IAW A300 AMM 55-12-11/401. REMOVED APRON SUPPORT BEHIND PANEL 333AL AT HORIZONTAL STABILIZER TO FOM IAW A300 AMM 55-15-13/401. INSTALLED 1 EA NEW APRON SUPPORT IAW SA300-600-SRM-51-40-21-001. INSTALLED SUPPORT BEHIND PANEL 333AL AT HORIZONTAL STABILIZER I.A.W. A300-600 AMM 55-12-11/401. RE-INSTALLED L/H LEADING EDGE PANEL 331A IAW A300 AMM 55-12-11/401.