DOC AIRBUS | AMM A320FENGINE INDICATING - GENERAL - DESCRIPTION AND OPERATION
** ON A/C NOT FOR ALL
1. General
The engine power management indicating is performed by means of:
** ON A/C NOT FOR ALL The engine power management indicating is performed by means of:
- the ECAM system (upper and lower display units)
- the warning and caution systems.
- the EEC and the ECAM
- the vibration monitoring system with a display on the ECAM.
- the engine management main parameters (N1, EPR LIMIT, EPR THROTTLE, EPR MAX, EPR REF)
- the engine vibration monitoring system.
- 73-30-00 for the fuel flow and the fuel filter clogging
- 79-00-00 for the oil parameters
- 75-00-00 for the nacelle temperature
- 78-30-00 for the thrust reverser indicating.
2. Component Location
** ON A/C NOT FOR ALL 
Control and Indicating - Component Location| ------------------------------------------------------------------------------- |
| FIN I FUNCTIONAL DESIGNATION I PANEL I ZONE I ACCESS I ATA |
| I I I I DOOR I REF. |
| ------------------------------------------------------------------------------- |
| 4013KS SENSOR-N1 77-11-00 |
| 4005EV PMA-EEC 77-11-00 |
| 4004EV TRANSDUCER UNIT-VIBRATION 77-32-15 |
| 2EV EVMU 86VU 128 824 77-32-34 |
| 4012KS1 THERMOCOUPLE-EGT,1 77-21-15 |
| 4012KS2 THERMOCOUPLE-EGT,2 77-21-15 |
| 4012KS3 THERMOCOUPLE-EGT,3 77-21-15 |
| 4012KS4 THERMOCOUPLE-EGT,4 77-21-15 |
| 4000EV SENSOR-EVMU N1 |
3. Indicating
A. Upper ECAM Display Unit
- N1
- EPR LIMIT
- EPR THROTTLE
- EPR MAX
- EPR REF
- EGT
- N2
B. Lower ECAM Display Unit
The VIB indication is normally green. If the advisory level is reached, the indication flashes (0.6 s bright and 0.3 s normal).
The VIB indication is normally green. If the advisory level is reached, the indication flashes (0.6 s bright and 0.3 s normal).