What was found
DURING HMV, CORROSION AROUND FASTENER TOP RIGHT-WING SURFACE STR 11 HEAR SLAT #3 DOT 88-023 ; REMOVED CORROSION FROM AREA IAW A320 SRM 57-21-11 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL THICKNESS .166 MATERIAL REMAIN .155 WITH A LOSS OF .011AND FOUND OUT OF LIMITS IAW A320 NTM 51-10-04 AND SRM 57-21-11-283-014. REPAIR OF AREA ACCOMPLISHED ON AND PER FAS EA#21066 REV IR AND JETBLUE EC#A21-986-01 APPROVED BY AIRBUS RDAF 80959978/006/2021 ISSUE A AS A PERMANENT REPAIR WITH INSPECTION REQUIREMENTS ( SEE APPENDIX A RDAF FOR INSPECTION INSTRUCTIONS) ALL WORK ACCOMPLISHED ON FAS NR-00148 W/O N580JB-03-01