As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK DAMAGE (0.25 INCH) WAS FOUND ON THE RH AND LH GUSSETS (P/N L533M1033201 LH / L533M1034201 RH) AND CORROSION WAS FOUND ON 40% OF FRAME 1 (P/N L533M101104).DAMAGE AND CORROSION WAS FOUND DURING 1000 HOUR INSPECTION. THE DAMAGE WAS REPAIRED VIA PART REPLACEMENT AND REPAIR IAW AIRBUS RDAS AHI 135 53 041 19 REV A.