W DOC AIRBUS | AMM A320F

ENGINE INDICATING - GENERAL - DESCRIPTION AND OPERATION

** ON A/C NOT FOR ALL
1. General
F Power Plant Indicating - General ** ON A/C NOT FOR ALL
The engine power management is effected by means of :
  • the ECAM system (upper and lower display units of the ECAM system)
  • the warning and caution systems.
The engine monitoring is carried out by means of :
  • the ECU and the ECAM
  • the vibration monitoring system with a display on the ECAM.
This chapter deals only with :
  • the engine management main parameters (N1, N1 LIM, N1 MAX, N1 REF, N1 CMD, N2 and EGT)
  • the engine vibration monitoring system of the engine.
The other engine parameters are described in the other ATA chapters :
The AIDS system (Ref. AMM D/O 31-36-00-00) receives the engine monitoring parameters through the FADEC (Ref. AMM D/O 73-20-00-00).
** ON A/C NOT FOR ALL
2. Component Location
F Control and Indicating - Component Location ** ON A/C NOT FOR ALL
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FIN I FUNCTIONAL DESIGNATION I PANELIZONEIACCESS I ATA
I I I I DOOR I REF.
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4000EV SENSOR-N1 ROTATIONAL SPD 77-11-10
4001EV SENSOR-N2 ROTATIONAL SPD 77-11-20
4002EV ACCLRM-No. 1 BRG VIB 77-31-10
4003EV SENSOR-TRF VIB 77-31-30
2EV EVMU 86VU 128 824 77-32-34
T495 THERMOCOUPLE 77-21-10

** ON A/C NOT FOR ALL
3. Indicating
A. General
The engine primary parameters are permanently displayed on the upper ECAM E/WD.
The secondary parameters are displayed on the lower ECAM DU when selected automatically or manually.
(1) Upper Display Unit of the ECAM System
F Upper Display Unit of the ECAM System ** ON A/C NOT FOR ALL
(2) Lower Display Unit of the ECAM System
F Lower Display Unit of the ECAM System - Engine Pages ** ON A/C NOT FOR ALL
[Rev.10 from 2021] 2026.04.02 06:37:39 UTC
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