What was found
(CAN)ON LANDING ROLL CREW FELT A HEAVY SHIMMY AND VIBRATION FROM THE LANDING GEAR. ON FINAL ROLL OUT, THE AIRCRAFT SETTLED LOWER ON THE L/H SIDE, HOWEVER, DIRECTIONAL CONTROL WAS MAINTAINED AND THE AIRCRAF T CAME TO A STOP IN THE CENTRE OF THE RUNWAY. THE L/H MLG WHEEL ASSEMBLIES AND BRAKE ASSEMBLIES HAD SEPARATED FROM THE STRUT. THE WHEEL ASSEMBLIES HAD IMPACTED THE L/H INBOARD FLAP - TWO LOCATIONS - CAUSING SUBSTANTIAL DAMAGE, AND ON AIRCRAFT STOPPING IMPACTED THE L/H OUTBOARD FLAP BRINGING THE WHEELS TO A HALT.