What was found
NR 2 ENGINE AFT STRUT FAIRING STIFFENER HAS 4 EACH ELONGATED HOLES FORWARD SIDE. REAMED HOLES TO .328 AND INSTALLED OVERSIZED FATSENERS IAW EA 25-154-02693 REFERENCE TASK TTG8Q015HNDM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 ENGINE AFT STRUT FAIRING STIFFENER HAS 4 EACH ELONGATED HOLES FORWARD SIDE. REAMED HOLES TO .328 AND INSTALLED OVERSIZED FATSENERS IAW EA 25-154-02693 REFERENCE TASK TTG8Q015HNDM.