What was found
DURING HMV, CORROSION AROUND FASTENER ROW TOP RIGHT WING SURFACE STR 11 BETWEEN RIB 3/4 ; REMOVED CORROSION IAW A320 SRM 51-74-00 PERFORMED NDT INSPECTION ON AREA WITH ORIGINAL THICKNESS .210 MATERIAL REMAIN .173 WITH A LOSS OF .037 AND FOUND OUT OF LIMITS IAW A320 NTM 51-10-08 AND SRM 57-21-11-283-014 REPAIR OF AREA ACCOMPLISHED ON AND PER FAS EA#21066 REV IR AND JETBLUEEC#A21-986-01 APPROVED BY AIRBUS RDAF 80959978/006/2021 ISSUE A AS A PERMANENT REPAIR WITH INSPECTION REQUIREMENTS (SEE APPENDIX A OF RDAF FOR INSPECTION INSTRUCTIONS) ALL WORK ACCOMPLISHED ON FAS NR-00141 W/O N580-03-01