What was found
DURING INSPECTION, FOUND DAMAGE IN THE FORM OF CORROSION TO THE STA1672.5 FRAME WEB (PN: B531K1323-209), FRAME 1 DESCRIPTION OF WORK: REPAIRED THE DAMAGE IN ACCORDANCE WITH AIRBUS REPAIR DESIGN APPROVAL RDAS-BK117-53-2022-0134A ISSUE A DATED 20 JAN 2022. APPROVED DATA: RDAS-BK117-53-2022-0134A ISSUE A DATED 20 JAN 2022 IS EASA APPROVED (DOA EASA.21J.700). IAW THE FAA AND EASA BILATERAL AGREEMENT AND TECHNICAL IMPLEMENTATION PROCEDURES, THE FAA CONSIDERS THE DATA FAA APPROVED.