What was found
(CAN) RIGHT AFT RUDDER CONTROL CABLE SWAGED CLEVIS BENT AND BUCKLED. THIS HAD CAUSED CABLE STRAND SEPARATION AND FRAYING. FURTHER INSPECTION FOUND THE RIGHT CABLE CLAMP P/N 2613397-2 LOOSE ON THE CABLE, LEADING TO A NO-LOCK CONDITION ON THE RIGHT RUDDER CONTROL CABLE WHEN THE CONTROL LOCK WAS DEPLOYED. THE AIRCRAFT HAD BEEN PARKED OUTSIDE DURING STRONG WIND CONDITIONS. THIS ALLOWED WIND TO MOVE RUDDER AGAINST ITS MECH STOP IN THE RIGHT HAND DIRECTION ONLY. THIS UNLOADED THE RIGHT RUDDER CABLE TENSION ALLOWING CABLE END CLEVIS TO SWING ABOUT ITS BOLTED CENTER; THUS, THE CLEVIS FORWARD END FOULED THE CABLE CUT-OUT ON BULKHEAD ASSY P/N 2612059-1 AT STA 427.88 AND BENDING THE CLEVIS.