Planetary gear system arrangement with auxiliary oil system

A gas turbine engine comprising:

• a fan shaft diving a fan having fan blades;
• a gear system including a sun gear surrounded by a plurality of intermediate gears, a carrier at least partially supporting said plurality of intermediate gears, and a ring gear surrounding said plurality of intermediate gears, wherein said sun gear is driven by a turbine;
• at least one fan shaft support bearing located forward of the gear system;
• a coupling fixing said ring gear from rotation relative to an engine static structure;
• and
• a lubrication system for lubricating components across a rotation gap, the lubrication system including a lubricant input, a stationary first bearing receiving lubricant from said lubricant input and having a first race in which lubricant flows, and a second bearing for rotating within said first bearing, said second bearing having a first opening in registration with said first race such that lubricant may flow from said first race through said first opening into a first conduit, wherein the stationary first bearing is located radially outward from a central axis of the second bearing with respect to an engine axis.