MANIFOLD FOR GEARED TURBOFAN ENGINE

A geared architecture (48) for a gas turbine engine (20) includes a lubricant manifold (76) for directing lubricant flow to the geared architecture (48). The manifold (76) including annular channel (80, 84) and a bowl member (82, 86) received within the annular channel (80, 84) for defining a passage for directing lubricant.