As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENG STRUT - PYLON AFT BULKHEAD INTERIOR - HORIZONTAL STIFFENER CRACKED AT LOWER FLANGE, AT SECOND FASTENER FROM O/B END, APPROX 18 INCHES BELOW WING PLANK. REMOVED NR 1 ENG STRUT AFT FAIRING HORIZONTAL STIFFENER 18 INCHES BELOW WING PLANK ON AFT SIDE INTERIOR AND INSTALLED A NEW STIFFENER PER SRM 51-40-02.