What was found
DURING THE STRUCTURAL INSPECTION PER ZL-500-03-1-002 CORROSION WAS FOUND AT LH WING REAR SPAR T/E OVERHANG AREA BETWEEN RIB 10 AND RIB 11+186MM ADDITIONAL CORROSION ON THE OVERHANG TOP SKIN LOWER SURFACE WAS NOTED AND A ZERO STRESS JACKING WITH SKIN SEPARATION PROCESS WAS NECESSARY. COOPESA ASSESSED THE DAMAGE AND COORDINATED A REPAIR WITH AIRBUS VIA TECHREQUEST DOSSIER # 81110525, TD81110525/057/2022#B, R572-58616 ISSUE L, R572-58944 ISSUE E& R572-58943 ISSUE E.AIRBUS ISSUED A REPAIR APPROVAL BY MEANS OF RDAF REF 81110525/082/2022#A. THE APPROVED REPAIR PROCEDURE IS CAPTURED IN COOPESA EO # COO-EO-2023-1|6311-R01