What was found
#2 ENGINE LOWER AFT PYLON; AFT WEDGE HAS A CRACK APPROXIMATELY .8 LONG.<[01] VERIFIED CRACK WITH HFEC PER NDT PART 6 51-00-00 PROCEDURE 23.;[02] REPAIRED PER EA# M-23-154-01884
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
#2 ENGINE LOWER AFT PYLON; AFT WEDGE HAS A CRACK APPROXIMATELY .8 LONG.<[01] VERIFIED CRACK WITH HFEC PER NDT PART 6 51-00-00 PROCEDURE 23.;[02] REPAIRED PER EA# M-23-154-01884