Bearing System for Gas Turbine Engine

A bearing system (38A) for a gas turbine engine includes a spring (62) defined about an axis of rotation. The spring (62) has a multiple of beams (82) which extend between a flange structure (84) and an attachment structure (86). A damper (64) is defined about the axis of rotation and mounted to the spring (62) to at least partially axially overlap the multiple of beams (82).