The in-line booster pump overpumps the fuel from the tank to the main engine fuel pump. It can be used for turbine or piston engine applications operating with all typical A/C fuels and additives.
The booster pump is of modular design consisting of a fuel pumping stage, electric motor, and analog motor control. A non-return valve can be mounted at the discharge port. The fuel pumping stage is a centrifugal pump consisting of an impeller and stator
Fuel transfer system
Ensures the supply of fuel to the engine or its interruption, maintaining fuel levels in the tanks, filtering fuel and more... and thus ensures the safe operation of the aircraft.
