As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REPAIR - CRACK; #2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY<[01] REMOVED TRAILING EDGE FITTING;[02] REMOVED AND REPLACED AFT. END STRUT FARING SEGMENT PER SRM 51-20-02.;[03] CORRECTIVE ACTION STEP 2. IT SHOULD BE: <BR>REMOVED AND REPLACED AFT. END STRUT FARING SEGMENT PER SRM 51-40-02.<BR>APPLIED SURFACE FINISH PER AMM 51-21-99;[04] C/W