What was found
DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FASTENER HOLE (AFT-LOWER POSITION) LOCATED ON FR35 AT S30L, LOWER FUSELAGE. CRACK DEPTH = 0.100 INCHES APPROX, CRACK POSITION: 5 AND 11 OCLOCK, LOOKING FROM OUTSIDE. REF AEROMAN WO 2026 244/1 NR 2026-301086. PERFORMED REPAIR ON HOLE (H2) LOCATED ON FR35 AT LEVEL OF STR30 LH SIDE ON LOWER FUSELAGE IAW EA 53-0047-26, EC AND RDAF 81807254/007/2026 ISSUE B. AIRBUS APPROVED THE REPAIR AS INTERIM WITHOUT CATEGORY.