As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING B CHECK INSP, VISUAL INSP OF CABLE SYS, THE RT FLAP INTERCONNECT CABLE IS WORN BEYOND LIMITS JUST OTBD OF NR 2 NACELLE. WS 91.20 PANEL 841-3. WHEN THE FLAP IS IN THE UP POSITION THE CABLE VIBRATED IN THE FAIRLEAD HOLE CAUSING WEAR. THE MICARTA IS TO BE OPENED TO ALLOW PROPER CLEARANCE.