What was found
#1 ENG PYLON AFT STRUT FAITING SUPPORT FITTING CRACKED INTO RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROC 23.COMPLIED WITH E.A 21-154-02194. PERFORM REPETITIVE INSPECTIONS EVERY 8 DAYS AND PERMANENT REPAIR WITHIN 60 DAYS PER EA 21-154-02194.PERFORM GENERAL VISUAL INSPECTION ON END OF CRACK FOR ANY PROGRESSION. IF DEFECTS ARE NOTED CONTACT ENGINEERING. PER EA 21-154-02194.REPETITIVE ACTION REQUIRED. /