Power transfer units (PTUs) are used to transfer hydraulic power from one hydraulic system to another without mixing fluid. PTUs are generally used for a contingency purpose or as a ground service source of hydraulic power....
This electric motor-driven cooling pump assembly has two motor pumps for either redundancy or dual flow operation....
This electric motor-driven gear pump assembly meters fuel directly to a gas turbine engine fuel manifold and nozzles....
Parker Aerospace engine feed ejector pumps are hydro-mechanical jet pumps, with no moving parts. The pumps independently supply fuel to their respective engines using the motive flow supplied by the engine...
The electric motor-driven pump (EMP) is liquid cooled to increase the efficiency of the motor cooling for aircraft-specific applications, where the flow can be easily adjusted to meet the needs of your application....
Parker Aerospace pressure refuel caps are used to lock, seal and vent the pressure refuel port for an aircraft fuel tank. Pressure refueling allows for single-point refueling on larger aircraft....
Parker Aerospace lightning-safe gravity fuel filler caps are used to lock, seal, and act as an identifier for the gravity fill port of an aircraft fuel tank....
Parker Aerospace dual-wall transfer tube provides self-aligning capability in aerospace fuel system applications to compensate for linear and angular misalignment....