What was found
DURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE AFT LOWER COMMON TO SKIN, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.12 0 INCH, IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1458309 TASKCARD: NR-00066 ) REF AEROMAN WO 2026 280/1 NR 2026-346048 ACCOMPLISHED REPAIR OF CRACK AT FASTENER HOLES W1 (ONLY IN FR 35 WEB LAYER) HOLE #2 (FWD AND AFT SKIN ONLY) HOLE #3 (FWD AND AFT SKIN ONLY) AND HOLE #9 (GUSSET) AT THE CENTER FUSELAGE FR 35 PRESSURE BULKHEAD AT LEVEL OF THE STR 30LH IN ACCORDANCE WITH AEROMAN EA 53-0058-26 REV 0 (COVER AND PARTS 1-4) AND EC A26-646-01 FOR SOLUTION LIFE OR LIMITATION 6 MONTHS SEE AIRBUS RDAF 81829072/003/2026 ISSUE A.