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 /
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
#2 ENGINE; AFT STRUT FAIRING SUPPORT FITTING CRACKED THROUGH RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROCEDURE 23 /