What was found
#2 ENGINE; AFT STRUT FAIRING SUPPORT FITTING CRACKED THROUGH RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROCEDURE 23.C/W EA 21-154-02194 PREFORM REPETITIVE INSPECTION EVERY 8 DAYS AND PERMANENT REPAIR IN 60 DAYS. ACCOMPLISH OPTION 1 OR 2. PREFORM 737-800 SRM 54-50-70-2R-6 TO REPAIR THE CRACKED FLANGE IF ALL OTHER CRITERIA OF 737-800 SRM 54-50-70-2R; REPAIR 6 CAN BE MET. OPTION 2 REPLACE AFT FAIRING TRAILING EDGE ASSY. P/N 313A2752-1 OR THE REPLACEMENT PANEL P/N 313A2752-2 PER EA 21-154-02194.PERMANENT ACTION REQUIRED. /