What was found
DURING ROUTINE INSP HFEC IND THE LWR RUDDER, THRUST HINGE RIB FITTING WAS CRACKED AT FWD RIGHT SIDE. *S/D* REMOVED AND REPLACED RUDDER THRUST HINGE RIB PER IAW FEDEX EO 7-5550-7-2303C PART 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSP HFEC IND THE LWR RUDDER, THRUST HINGE RIB FITTING WAS CRACKED AT FWD RIGHT SIDE. *S/D* REMOVED AND REPLACED RUDDER THRUST HINGE RIB PER IAW FEDEX EO 7-5550-7-2303C PART 2.