Filter assembly for an aircraft engine

An aircraft engine, comprising:

• a fuel system including a fuel tank containing fuel for the aircraft engine and a fuel pump flow flowing the fuel to a combustor of the aircraft engine;
• an oil system including an oil tank containing oil for the aircraft engine and an oil pump for circulating the oil to components of the aircraft engine;
• and
• a filter assembly for the fuel system or the oil system, the filter assembly including a filter housing defining an inner cavity, the filter housing having a fluid inlet and a fluid outlet for flowing the fuel or the oil into and out of the inner cavity, a filter bowl removably attached to the filter housing to seal the inner cavity, and a filter disposed in the inner cavity for filtering the fuel or the oil, the filter electrically coupled to the filter bowl at a first electrical connection and the filter electrically coupled to the filter housing at a second electrical connection distinct from the first electrical connection to thereby indirectly electrically couple the filter bowl to the filter housing via the filter, one or both of the first electrical connection and the second electrical connection being compressible upon engagement with the filter.