What was found
DURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON STR 5 LH FR 74 PLUS 1 INCH .CRACK DIRECTION PARALEL TO RADIUS OF STRINGER.CRACK LENGTH 0.250INCH; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00069 ) REF AEROMAN W/O 2026 280/1 NR 346167. ACCOMPLISHED THE REPAIR OF CRACK DAMAGE ON THE REAR FUSELAGE TAILCONE ON STRINGER 5LH AT LEVEL OF FR74 IN ACCORDANCE WITH AEROMAN EA 53-0083-26 REV. 0 ( COVER AND PART 1 ) AND AIRBUS RDAF 81841016/003/2026 ISSUE B IAW EC NO. A26-695-01