DOC AIRBUS | AMM A320FFUEL FLOW INDICATING - DESCRIPTION AND OPERATION
** ON A/C NOT FOR ALL
1. General
The engine indicating system is part of the engine fuel and control system (Ref. AMM D/O 73-00-00-00).
** ON A/C NOT FOR ALL The engine indicating system is part of the engine fuel and control system (Ref. AMM D/O 73-00-00-00).
Fuel Flow Transmitter2. System Description
The engine indicating system gives the signals back to the Electronic Engine Control (EEC) regarding the overall engine condition.
** ON A/C NOT FOR ALL The engine indicating system gives the signals back to the Electronic Engine Control (EEC) regarding the overall engine condition.
3. Component Description
A. Fuel Flow Transmitter
The main function of the fuel flow transmitter is to measure the mass flow rate of fuel supplied to the combustor.
The fuel flow meter is located in line between the Fuel Metering Unit (FMU) discharge and the Split Control Unit/Servo Valve Assembly (SCU/SVA).
The main function of the fuel flow transmitter is to measure the mass flow rate of fuel supplied to the combustor.
The fuel flow meter is located in line between the Fuel Metering Unit (FMU) discharge and the Split Control Unit/Servo Valve Assembly (SCU/SVA).