W DOC AIRBUS | TSM A320F

Loss of the VOR 1 Data Bus Identified by the CFDS


TASK 34-55-00-810-806-A
Loss of the VOR 1 Data Bus Identified by the CFDS


1. Possible Causes
  • RECEIVER-VOR/MKR, 1 [3RS1]
  • wiring of the OMNI BEARING AND SIGNAL MKR OUTPUT 2 bus from the VOR/MKR receiver 1 (3RS1) 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 345501
AMM 34-55-31-000-001
Removal of the VOR/MKR Receiver
AMM 34-55-31-400-001
Installation of the VOR/MKR Receiver
3. Fault Confirmation
Subtask 34-55-00-865-053-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUNAV/VOR/12RS1G13
Subtask 34-55-00-740-060-A
B. Test
On the CFDS MENU page, get access to the AVIONICS STATUS page AMM 31-32-00-869-002.
4. Fault Isolation
Subtask 34-55-00-810-057-A
A. If the test gives the maintenance message NO VOR 1 DATA:
   (1) If the fault continues:
  • do a check and repair the wiring of the OMNI BEARING AND SIGNAL MKR OUTPUT 2 bus from the VOR/MKR receiver 1 (3RS1) to the first terminal block ASM 345501.
Subtask 34-55-00-740-061-A
B. Do the test given in Para. 3.B.
[Rev.8 from Aug 2018] 2026.04.04 04:33:29 UTC