As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 PYLON ATTACH ANGLE IS CRACKED O/B SIDE AFT OF O/B COWLS AFT HINGE FITTING AT STA NAC318. REMOVED NR 1 ENG EXHAUST SLEEVE IAW B767 MM 78-11-01. REPAIRED ATTACH ANGLE IAW B767 MM 51-40-02 & DRAWING 313T1380. RE-INSTALLED NR 1 EXHAUST SLEEVE IAW B767 MM 78-11-01, 1.0 INCH CRACK.