As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
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. PREFORM GVI ON END OF CRACK FOR ANY PROGRESSION. IF DEFECTS ARE NOTED CONTACT ENGINEERING. PER EA 21-154-02194.REPETITIVE ACTION REQUIRED. /