What was found
DURING PERFORMING A 3 YEAR CHECK AT SIAEP, AN OF INSPECTION AS PER B321-ZL-500-02-1, CORROSION WAS FOUND ON THE LT WING BOTTOM SKIN PANEL 2 BETWEEN RIBS 24-25. AFTER DAMAGE ASSESSMENT AS PER SRM 57-21-11-283-014, CONTACT WITH AIRBUS IS REQUIRED SINCE THE BLENDING OF THE CORROSION WILL EXTEND OVER A FASTENER. THIS RI-HAL-57-006 IS ISSUED TO EMBODY THE PERMANENT REPAIR OF THE DAMAGED AREA, WITH REFERENCE TO REPAIR DWG R572-58616 ISSUE M, WITH APPROVAL RDAF 81350928/004/2024-A.