What was found
RIGHT ENGINE AFT STRUT FAIRING STIFFENER COMMON TO THE #1 FRAME SUPPORT OUTBOARD 2 HOLES ARE ELONGATED DUE TO LOOSE FASTENERS / REMOVED AND REPLACED RIGHT STRUT FAIRING STIFFENER COMMON TO #1 FRAME SUPPORT PER SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT ENGINE AFT STRUT FAIRING STIFFENER COMMON TO THE #1 FRAME SUPPORT OUTBOARD 2 HOLES ARE ELONGATED DUE TO LOOSE FASTENERS / REMOVED AND REPLACED RIGHT STRUT FAIRING STIFFENER COMMON TO #1 FRAME SUPPORT PER SRM 51-40-02.