What was found
NR 1 PYLON AFT UPPER BULKHEAD "T" FRAME HAS A CRACK AT AFT FLANGE AND A SECOND CRACK AT FORWARD FLANGE, OUTBOARD OF NR 1 PYLON FRONT SPAR CHORD ASSEMBLY. AFT FLANGE CRACK IS 0.750 INCH LONG. FORWARD FLANGE CRACK IS 0.375 INCH LONG AT NACELLE STATION 270.00. ACCOMPLISHED INTERIM REPAIR AS PER 747-200 SRM 51-30-02 AND ATLAS AIR XEO NR 54-030107, FAA FORM 8110-3 ISSUED AND APPROVED. PERMANENT REPAIR TO BE ACCOMPLISH AT NEXT "C" CHECK.