What was found
THE NR 2 PYLON STRUT SKIN IS CRACKED AT THE FORWARD ACCESS HOLE ON THE O/B SIDE. THE CRACK IS .875 INCH LONG OUT OF THE UPPER AFT CORNER. THE SKIN IS AN 0.080 PLUS 0.080 CLAD 2024-T3 BONDED ASSEMBLY. DFW MX IS ACCOMPLISHING A REPAIR PER B767-300 SRM 54-53-01, BUT DO NOT HAVE THE EQUIPMENT NECESSARY TO COLD-WORK THE STOP DRILL HOLE. THIS ER/A AUTHORIZES DEFERRAL OF THE COLD-WORKING. RESTRICTIONS, HFEC INSPECT AND COLD WORK WITHIN 550 FLIGHT CYCLES; PERM REPAIR AT NEXT MID-VISIT; HFEC INSPECT HOLE EVERY 550 FLIGHT CYCLES.