What was found
THE CRACK FOUND IN THE TRANSITION RADIUS OF THE RIGHT FUSELAGE FRAME STUB BEAM LOCATED STA 883.5 AND RBL 89. THE CRACK WAS FOUND DURING A REPETITIVE HFEC SURFACE INSPECTION IAW BOEING SERVICE BULLETIN 767-53A0209, AS MANDATED BY AIRWORTHINESS DIRECTIVE 2012-22-17. THE REPAIR IS DEFINED WITHIN THIS ENGINEERING ORDER FOR STA 883.5 IS IAW BOEING SERVICE BULLETIN 767-53A0209 REVISION 2 AS MANDATED BY AD 2012-22-17.