As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT ENGINE AFT PYLON AFT A-FRAME IS CRACKED. CRACK ORIGINATES AT FRAME DOUBLER AND CONTINUES THROUGH RADIUS FOR OVERALL LENGTH OF 1.2 INCHES. VERIFIED WITH NDT PART 6 PROCEDURE 23.<[01] 04 - REPAIRED PER [EA M-23-154-01884-REPREF (737-700/-800 - SWA-REPAIR- CRACK; #1/#2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY- REPAIR REFERENCE)]