What was found
FITTING CRACKED AT VERTICAL WEB AT LEFT ENGINE PYLON STRUCTURE, VIEWED THROUGH PANEL 8105A. REMOVED AND REPLACED FITTING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FITTING CRACKED AT VERTICAL WEB AT LEFT ENGINE PYLON STRUCTURE, VIEWED THROUGH PANEL 8105A. REMOVED AND REPLACED FITTING.