What was found
#2 ENG. AFT STRUT FAIRING. AFT FITTING IS CRACKEDCOMPLIED WITH WORK INSTRUCTION NO. REPAIR-54EA-07244. GENERAL VISUAL INSPECTION MUST BE PERFORMED AT THE END OF CRACK FOR ANY PROGRESSION EVERY 8 DAYS (NOTE PANEL #444BR MUST BE REMOVED TO PERFORM STOP DRILL GVI) PERMANENT REPAIR MUST BE COMPLIED WITH WITHIN 60 DAYS CONSISTING OF REPAIR OR REPLACEMENT OF; CRACKED AFT TRAILING EDGE ASSY (P/N 313A2752-1) OR REPLACEMENT PANEL (P/N313A2752-2) AMT 59828INSP 26613PERMANENT ACTION REQUIRED:ACCOMPLISH OPTION 1 OR OPTION 2: OPTION 1: PERFORM 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-6; REPAIR 6 CAN BE MET. OPTION 2: REPLACED AFT FAIRING TRAILING EDGE ASSEMBLY (P/N313A2752-1) OR THE REPLACEMENT PANEL (P/N313A2752-2). / REMOVED AND REPLACED THE AFT STRUT FAIRING TRAILING EDGE WEDGE PER SRM 51-40-02AMT 102665