DOC AIRBUS | AMM A320FFUEL FILTER WARNING SYSTEM - DESCRIPTION AND OPERATION
** ON A/C NOT FOR ALL
1. Component Location
The fuel filter differential sensor has one independent circuit that is installed on the side of the fuel manifold, next to the fuel filter.
** ON A/C NOT FOR ALL The fuel filter differential sensor has one independent circuit that is installed on the side of the fuel manifold, next to the fuel filter.
| FIN | FUNCTIONAL DESIGNATION | PANEL | ZONE | ACCESS DOOR | ATA REF |
|---|---|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||||
| 4002KS | FUEL FILTER DIFF PRESS SENSOR | 400 | 73-11-00 | ||
2. Component Description
A. Fuel Filter Differential Pressure Sensor
Engine Fuel and Control System - (IFPC, Fuel Filter Differential Pressure Sensor and Fuel Manifold)(1) The fuel filter differential pressure sensor measures the differential pressure across the fuel filter. If the fuel filter becomes clogged, the fuel filter differential sensor sends a signal through the Electronic Engine Control (EEC) that warns the ECAM display units in cockpit.
(2) The sensor has one independent circuit that is installed on the side of the fuel manifold, next to the fuel filter.