What was found
CRACK DAMAGE WAS DISCOVERED ON FRAME # 5A AT FUSELAGE STATION 5,023MM. ONE CRACK WAS LOCATED AT THE FLANGE RADIUS WHERE THE FRAME MEETS THE OUTER STRUCTURE AT THE RH SIDE. THE CRACK WAS STOP DRILLED THEN RE-ENFORCED VIA AN AIRBUS REPAIR DOUBLER (PN: L533M1022966) IAW AIRBUS SERVICE BULLETIN EC135-53-031, INITIAL REVISION DATED 30 JUN 2014 AND MODIFIED TO FIT THE REPAIR AREA IAW AIRBUS SRM 51-71-53, 8-11, REVISION 11.00 DATED 25 JAN 2022