FLUID ADDITIVE SYSTEM

A lubrication system (60) for a gas turbine engine (20) includes a primary fluid tank (62) to receive a primary fluid, at least one secondary fluid tank (64) to receive at least one fluid additive, and a mixer (66). The mixer (66) has at least a first inlet (68) in fluid communication with the primary fluid tank (62) and a second inlet (70) in fluid communication with the at least one secondary fluid tank (64). The mixer (66) has at least one outlet (72) that delivers a mixture of the primary fluid and the at least one fluid additive to a gas turbine engine component (74).