What was found
DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 BULK HEAD LH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER OUTBOARD COMMON TO MILLED COUPLING, CRACK DIRECTION ARE 4 AND 9OCLOCK, CRACKDEPTH IS 0.120 INCHAPOROX., IN FWD CARGO COMPARTMENT (2EA); (RESOLVED ON W/O: 1435456 TASKCARD: NR-00047 ) REF AEROMANW/O 2026 279/1 NR 348543 ACCOMPLISHED MAJOR REPAIR OF THE REPORTED CRACK AT THE FR35 LHS AT HOLE #2 ON FWD AND AFT SKIN LAYERS AND AT HOLE #W1 ON THE FR35 WEB LAYER I.A.W.AEROMAN EA 53-0055-26 REV.0 (COVER PARTS 1-6) SOLUTION LIFE OR LIMITATION: 6 MONTHS IAW AIRBUS RDAF 81825284/003/2026#A AND EC NO.A26-710-01.