Electric motor driven auxiliary oil system for geared gas turbine engine

A gas turbine engine comprising:

• a propulsor drive turbine, a propulsor rotor, and a gear reduction driven by said propulsor drive turbine and, in turn, to drive said propulsor rotor, a main oil supply system for supplying oil to components within said gear reduction, and an auxiliary oil supply system;
• an auxiliary oil tank having an overflow conduit that allows excess oil to fall to the bottom of a bearing compartment;
• said auxiliary oil tank positioned at a vertically higher location relative to an auxiliary oil pump;
• and
• said auxiliary oil tank having a tube with holes, and the holes positioned at a location such that oil may be drawn from said auxiliary oil tank when it is full or under negative gravity conditions, said tube connected through a first fluid connection to the auxiliary oil pump, and the overflow conduit being separate from the first fluid connection, said auxiliary oil pump also receiving oil from a sump through a second fluid connection.