As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN)DURING INSPECTION PHASE A SLIGHT BULGE IN THE SKIN ON THE OUTBOARD ENGINE NACELLE AT STN 135.O TO 171.0, WATER LINE 0.0 TO 111.0 BETWEEN RIVETS WAS DETECTED. AN NDT X-RAY REVEALED SLIGHT CORRO SION IN THE AREA OF THE RIVETS AND EXTENSIVE CORROSION ON A STRINGER REMOVED FROM THIS AREA. REPAIRS TO THIS AREA OF CORROSION CARRIED OUT.