What was found
DURING COMPLIANCE OF AD 75-14-06, AD 90-18-03; SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND A CRACK INDICATION ON THE NR 2 ENGINE UPPER OUTBOARD THRUST REVERSER DRIVER LINK. REMOVED LINK IAW DC-9 MM 78-31-5. LINK CRACKED, SCRAPPED LINK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING COMPLIANCE OF AD 75-14-06, AD 90-18-03; SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND A CRACK INDICATION ON THE NR 2 ENGINE UPPER OUTBOARD THRUST REVERSER DRIVER LINK. REMOVED LINK IAW DC-9 MM 78-31-5. LINK CRACKED, SCRAPPED LINK.