What was found
NR 2 ENG I/B CORE COWL AFT HINGE ARM ATTACH ANGLE IS CRACKED AND FASTENERS LOOSE. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-30-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 ENG I/B CORE COWL AFT HINGE ARM ATTACH ANGLE IS CRACKED AND FASTENERS LOOSE. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-30-02.