W DOC AIRBUS | TSM A320F

Loss of the EVMU Output Bus


TASK 77-30-00-810-830-A
Loss of the EVMU Output Bus


1. Possible Causes
  • EVMU [2EV]
  • wiring from the EVMU (2EV) pins AA/13A, 13C to the first terminal block
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 31-32-00-869-002
Procedure for the Class 3 Fault Reading
ASM 773202
AMM 77-32-34-000-040
Removal of the Monitoring Unit Engine Vibration (EVMU)
AMM 77-32-34-000-042
Removal of the Engine Vibration Monitoring Unit (EVMU)
AMM 77-32-34-400-040
Installation of the Vibration Monitoring Unit (EVMU)
AMM 77-32-34-400-042
Installation of the Engine Vibration Monitoring Unit (EVMU)
3. Fault Confirmation
Subtask 77-30-00-865-050-A ** ON A/C NOT FOR ALL
A. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUENGINE/ENG1 AND 2/EVMU1EVR44
Subtask 77-30-00-740-050-A ** ON A/C NOT FOR ALL
B. Test
On the CFDS MENU page, get access to the AVIONICS STATUS page AMM 31-32-00-869-002.
4. Fault Isolation
Subtask 77-30-00-810-075-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message NO EVMU DATA:
   (1) If the fault continues:
  • do a check and repair the wiring from the EVMU (2EV) pins AA/13A, 13C to the first terminal block ASM 773202.
Subtask 77-30-00-810-075-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message NO EVMU DATA:
   (1) If the fault continues:
  • do a check and repair the wiring from the EVMU (2EV) pins AA/13A, 13C to the first terminal block ASM 773202.
Subtask 77-30-00-740-051-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:37:47 UTC