Mechanical pump back-flow valve?
The fuel system design of a particular aircraft tees the electric boost pump output directly into the line that feeds the carbs - which is the pressurized side of the mechanical pump. So, it is important to understand if the mechanical pump is capable of allowing back-flow if it should fail.
I know this config is a little different than Rotax factory recommendations, that's not at issue. I'm asking from a purely technical perspective.
Thanks!