What was found
DURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE FWD MIDDLE COMMON TO SKIN,CRACK DIRECTION IS 12OCLOCK, CRACK DEPTH IS0.085INCH,IN FWD CARGO COMPARTMENT (1EA) ; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00070 ) REF AEROMAN WO 2026-280/1, NR 2026 - 346046, ACCOMPLISHED REPAIR OF CRACK AT HOLE #3 (FWD AND AFT SKIN ONLY) AT THE CENTER FUSELAGE FR 35 PRESSURE BULKHEAD AT LEVEL OF THE STR 30LH IN ACCORDANCE WITH AEROMAN EA 53-0058-26 REV O (COVER AND PARTS 1-4) AND EC A26-646-01 FOR SOLUTION LIFE OR LIMITATION IS FOR 6 MONTHS SEE AIRBUS RDAF 81829072/003/2026 ISSUE A