What was found
TORQUE LINK ATTACH POINT ON THE RIGHT STRUT BROKE AT LANDING. THIS ALLOWED THE RIGHT MLG TIRE TO ROTATE AND PULL THE AIRCRAFT OFF THE RUNWAY. THE RESULTING SIDE LOAD ON THE MLG CAUSED THE OVER CENTER LINK PN 400084-001, AND THE STRUT CYLINDER 400054-001, TO BREAK. ALSO, BOTH RIGHT SIDE MLG DOOR WERE DAMAGED ALONG WITH THE RIGHT FLAP. THE CUFF FOR ATTACHING THE TORQUE LINKS TO THE STRUT IS INSTALLED BY THE SWEAT METHOD. IN THIS CASE, THE CUFF WAS BROKEN AT THE ATTACH POINT FOR THE SCISSORS LINK FOR SOME TIME AND NOT NOTICED DUE TO COVERAGE OF PAINT. IT TOOK A FEW LANDINGS FOR THE SWEAT ATTACHMENT TO BREAK LOOSE. THE DISBONDING WAS EVIDENT BY THE DISCOLOR OF THE SWEAT SEALED AREA ON THE CUFF AND THE STRUT.